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Relevant bibliographies by topics / Aerospace engineering

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Academic literature on the topic 'Aerospace engineering'

Author: Grafiati

Published: 4 June 2021

Last updated: 30 July 2024

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Journal articles on the topic "Aerospace engineering"

1

Zalewski, Janusz. "Aerospace software engineering." Control Engineering Practice 3, no. 9 (September 1995): 1349–50. http://dx.doi.org/10.1016/0967-0661(95)90053-5.

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English, Lyn D., Donna T. King, Peter Hudson, and Les Dawes. "The Aerospace Engineering Challenge." Teaching Children Mathematics 21, no. 2 (September 2014): 122–26. http://dx.doi.org/10.5951/teacchilmath.21.2.0122.

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Integrating Science, Technology, and Engineering in Mathematics authors share ideas and activities that stimulate student interest in the integrated fields of science, technology, engineering, and mathematics (STEM) in K—grade 6 classrooms. This article describes an activity that introduced fourth-grade students to the work of aerospace engineers and to the science, technology, and mathematics principles associated with flight.

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Fryer, T. "Blast Off! [Aerospace Engineering]." Engineering & Technology 13, no. 1 (February 1, 2018): 34–36. http://dx.doi.org/10.1049/et.2018.0101.

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Valenti, Michael. "Re-Engineering Aerospace Design." Mechanical Engineering 120, no. 01 (January 1, 1998): 70–72. http://dx.doi.org/10.1115/1.1998-jan-5.

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This article reviews that by integrating its CAD/CAM tools, Boeing’s Space Systems Unit hopes to enhance the quality of its products as it reduces both design- and manufacturing-cycle times. Sharper market competition led management to re-emphasize the practice and couple it with integrated CAD/CAM systems to provide a more supportive environment for concurrent engineering, thereby assuring the customer that cost, schedule, and quality goals would be met. This concept, called integrated product development (IPD), was launched in 1991. Boeing’s intention is to use the IPD strategy to reduce design-cycle time and manufacturing-cycle time as well as recurring costs. To support IPD, the Boeing designers developed electronic change control (ECC), an online system that enables engineers, technicians, manufacturers, and logisticians throughout the company to track and control engineering changes on a network of minicomputers, workstations, and desktops. Among the Unigraphics-based tools Boeing uses in IPD is the electronic development fixture (EDF), a three-dimensional digital model. EDF enables its users to electronically investigate fit, form, function, and interference detection.

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Scott, R. Neil. "Sources: Encyclopedia of Aerospace Engineering." Reference & User Services Quarterly 50, no. 4 (June 1, 2011): 396–97. http://dx.doi.org/10.5860/rusq.50n4.396.

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Fryer, T. "Life on Mars [Aerospace Engineering]." Engineering & Technology 13, no. 1 (February 1, 2018): 42–46. http://dx.doi.org/10.1049/et.2018.0103.

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Mertins, Kseniya, Veronica Ivanova, Natalya Natalinova, and Maria Alexandrova. "Aerospace engineering training: universities experience." MATEC Web of Conferences 48 (2016): 06002. http://dx.doi.org/10.1051/matecconf/20164806002.

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Silvestrini, Rachel T., and Peter A. Parker. "Aerospace Research through Statistical Engineering." Quality Engineering 24, no. 2 (April 2012): 292–305. http://dx.doi.org/10.1080/08982112.2012.641146.

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Arpentieva, Mariam, Olga Duvalina, and Irina Gorelova. "Intersubjective management in aerospace engineering." MATEC Web of Conferences 102 (2017): 01002. http://dx.doi.org/10.1051/matecconf/201710201002.

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Mahadevan, Sankaran. "Probabilistic Methods for Aerospace Engineering." Journal of Aerospace Engineering 14, no. 4 (October 2001): 119. http://dx.doi.org/10.1061/(asce)0893-1321(2001)14:4(119).

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Dissertations / Theses on the topic "Aerospace engineering"

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Figueroa, Leonard J. "Aerospace Intrapreneurship: Systems Engineering an Aerospace Front End." Digital Commons at Loyola Marymount University and Loyola Law School, 2017. https://digitalcommons.lmu.edu/etd/394.

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Pratt, Roger W. "Control problems in aerospace engineering." Thesis, Loughborough University, 1995. https://dspace.lboro.ac.uk/2134/27604.

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Control Engineering is a wide-ranging discipline which offers opportunities in research to people with diverse backgrounds and interests; from applied mathematicians interested solely in developing new theory right through to pragmatic engineers who are closely involved in a particular application. Additionally, for those involved in the application of control methodologies, there are the bonuses of complementing modelling, analysis and design with experimental validation. For my part, work has centred on the application of existing techniques in new areas. Since the early part of my career were spent in the aircraft industry and the Royal Air Force, it has proved very satisfying to return to this area after some years in 'general' control engineering.

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Marvasti, Mazda Alim. "Applications of fractal geometry in aerospace engineering." Diss., Georgia Institute of Technology, 1991. http://hdl.handle.net/1853/12079.

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Jenett, Benjamin (Benjamin Eric). "Digital material aerospace structures." Thesis, Massachusetts Institute of Technology, 2015. http://hdl.handle.net/1721.1/101837.

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Thesis: S.M., Massachusetts Institute of Technology, Department of Civil and Environmental Engineering, 2015.
Cataloged from PDF version of thesis.
Includes bibliographical references (pages 71-76).
This thesis explores the design, fabrication, and performance of digital materials in aerospace structures in three areas: (1) a morphing wing design that adjusts its form to respond to different behavioral requirements; (2) an automated assembly method for truss column structures; and (3) an analysis of the payload and structural performance requirements of space structure elements made from digital materials. Aerospace structures are among the most difficult to design, engineer, and manufacture. Digital materials are discrete building block parts, reversibly joined, with a discrete set of positions and orientations. Aerospace structures built from digital materials have high performance characteristics that can surpass current technology, while also offering potential for analysis simplification and assembly automation. First, this thesis presents a novel approach for the design, analysis, and manufacturing of composite aerostructures through the use of digital materials. This approach can be used to create morphing wing structures with customizable structural properties, and the simplified composite fabrication strategy results in rapid manufacturing time with future potential for automation. The presented approach combines aircraft structure with morphing technology to accomplish tuned global deformation with a single degree of freedom actuator. Guidelines are proposed to design a digital material morphing wing, a prototype is manufactured and assembled, and preliminary experimental wind tunnel testing is conducted. Seconds, automatic deployment of structures has been a focus of much academic and industrial work on infrastructure applications and robotics in general. This thesis presents a robotic truss assembler designed for space applications - the Space Robot Universal Truss System (SpRoUTS) - that reversibly assembles a truss column from a feedstock of flat-packed components, by folding the sides of each component up and locking onto the assembled structure. The thesis describes the design and implementation of the robot and shows that an assembled truss compares favorably with prior truss deployment systems. Thirds, space structures are limited by launch shroud mass and volume constraints. Digital material space structures can be reversibly assembled on orbit by autonomous relative robots using discrete, incremental parts. This will enable the on-orbit assembly of larger space structures than currently possible. The engineering of these structures, from macro scale to discrete part scale, is presented. Comparison with traditional structural elements is shown and favorable mechanical performance as well as the ability to efficiently transport the material in a medium to heavy launch vehicle. In summary, this thesis contributes the methodology and evaluation of novel applications of digital materials in aerospace structures.
by Benjamin Jenett.
S.M.

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Stimac, Andrew K. (Andrew Kenneth) 1977. "Precision navigation for aerospace applications." Thesis, Massachusetts Institute of Technology, 2004. http://hdl.handle.net/1721.1/16676.

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Thesis (S.M.)--Massachusetts Institute of Technology, Dept. of Mechanical Engineering, 2004.
Vita.
Includes bibliographical references (p. 162). Includes bibliographical references (p. 162).
This electronic version was submitted by the student author. The certified thesis is available in the Institute Archives and Special Collections.
Navigation is important in a variety of aerospace applications, and commonly uses a blend of GPS and inertial sensors. In this thesis, a navigation system is designed, developed, and tested. Several alternatives are discussed, but the ultimate design is a loosely-coupled Extended Kalman Filter using rigid body dynamics as the process with a small angle linearization of quaternions. Simulations are run using real flight data. A bench top hardware prototype is tested. Results show good performance and give a variety of insights into the design of navigation systems. Special attention is given to convergence and the validity of linearization.
by Andrew K. Stimac.
S.M.

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Aouf, Nabil. "Robust control techniques for aerospace vehicles." Thesis, McGill University, 2001. http://digitool.Library.McGill.CA:80/R/?func=dbin-jump-full&object_id=38145.

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The research work presented in this thesis deals with flight control problems. Based on robust control techniques such as H infinity control and mu-synthesis, we develop control laws that are efficient in reducing gust loads on flexible aircraft. Uncertainty models for flexible aircraft are proposed and shown to be well adapted for robust control design, while tightly covering unknown but bounded variations of flexible mode parameters. One of the models presented introduces a new complex-rational controller design methodology that takes advantage of the uncertain plant structure and achieves good performance criteria. Other uncertainty models are presented for the first time for the purpose of closed-loop reduction of flexible models. We propose a new model/controller order reduction method for flexible aircraft preserving robust performance in closed loop. Two case studies of complex aircraft are presented with the objective of full flight envelope control. Solutions for scheduled control laws are given to maintain performance objectives along the entire flight envelope. We adapt to our complex aircraft case study known gain scheduling techniques such as observer-form controller scheduling, and we propose new gain scheduling techniques, including a robust performance blending/interpolation design, an optimal multi-switching methodology and a scheduled-partitioned controller.

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Hart, Peter Bartholomew. "A plm implementation for aerospace systems engineering-conceptual rotorcraft design." Thesis, Georgia Institute of Technology, 2009. http://hdl.handle.net/1853/28278.

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The thesis will discuss the Systems Engineering phase of an original Conceptual Design Engineering Methodology for Aerospace Engineering-Vehicle Synthesis. This iterative phase is shown to benefit from digitization of Integrated Product&Process Design (IPPD) activities, through the application of Product Lifecycle Management (PLM) technologies. Requirements analysis through the use of Quality Function Deployment (QFD) and 7 MaP tools is explored as an illustration. A "Requirements Data Manager" (RDM) is used to show the ability to reduce the time and cost to design for both new and legacy/derivative designs. Here the COTS tool Teamcenter Systems Engineering (TCSE) is used as the RDM. The utility of the new methodology is explored through consideration of a legacy RFP based vehicle design proposal and associated aerospace engineering. The 2001 American Helicopter Society (AHS) 18th Student Design Competition RFP is considered as a starting point for the Systems Engineering phase. A Conceptual Design Engineering activity was conducted in 2000/2001 by Graduate students (including the author) in Rotorcraft Engineering at the Daniel Guggenheim School of Aerospace Engineering at the Georgia Institute of Technology, Atlanta GA. This resulted in the "Kingfisher" vehicle design, an advanced search and rescue rotorcraft capable of performing the "Perfect Storm" mission, from the movie of the same name. The associated requirements, architectures, and work breakdown structure data sets for the Kingfisher are used to relate the capabilities of the proposed Integrated Digital Environment (IDE). The IDE is discussed as a repository for legacy knowledge capture, management, and design template creation. A primary thesis theme is to promote the automation of the up-front conceptual definition of complex systems, specifically aerospace vehicles, while anticipating downstream preliminary and full spectrum lifecycle design activities. The thesis forms a basis for additional discussions of PLM tool integration across the engineering, manufacturing, MRO and EOL lifecycle phases to support business management processes.

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Austin, Mary Viva. "Improving Aerospace Engineering Laboratory Accessibility by Web Exporting Classes and Tasks." MSSTATE, 2005. http://sun.library.msstate.edu/ETD-db/theses/available/etd-04042005-044515/.

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In recent years, changes to the aerospace engineering curriculum have moved the laboratory classes ahead in the four year program. In an effort to alleviate the introduction of prerequisite and scheduling problems resulting from the curriculum changes, a study into the approach of making laboratory classes more accessible was initiated. Two options are in the process of being implemented as a solution to current and future curriculum obstacles as a result of this study. First, the first semester laboratory class has been successfully converted to an introduction to laboratory procedures class with the option of taking the lecture portion via the Web. Secondly, present preparations are underway to offer the entire introductory laboratory class via the Web. An in-depth analysis into laboratory tasks selected for the introductory class on laboratory procedures is presented, along with methods implemented, current results and suggestions for the future complete conversion into a virtual class.

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Levedahl, Blaine Alexander. "Decentralized Autonomous Control of Aerospace Vehicle Formations." NCSU, 2003. http://www.lib.ncsu.edu/theses/available/etd-03062003-104749/.

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Two approaches for the autonomous control of aerospace vehicle formations are developed. The development of the approaches relies on fundamental work in the areas of distributed control; specifically modal, robust, optimal, and decentralized control. The algorithms are shown to satisfy five separation principles that simplify design and enable the algorithms to be implemented reliably. The autonomous controllers uniformly dampen the modes of the formation (global control) using a decentralized approach and a nearest-neighbor approach. A numerical example illustrates robust formation changes from 9-vehicle (3 x 3) grids to V-type formations.

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Bennett, William Thomas. "Computational and Experimental Investigations into Aerospace Plasmas." Wright State University / OhioLINK, 2008. http://rave.ohiolink.edu/etdc/view?acc_num=wright1212780703.

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Books on the topic "Aerospace engineering"

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Blockley, Richard. Encyclopedia of aerospace engineering. Chichester, West Sussex, U.K: Wiley, 2010.

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Blockley, Richard, and W. Shyy. Encyclopedia of aerospace engineering. Chichester, West Sussex, U.K: Wiley, 2010.

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American Society of Civil Engineers. Aerospace Division. Journal of aerospace engineering. New York, N.Y: American Society of Civil Engineers, Aerospace Division, 1988.

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Academy, United States Naval, ed. Aerospace engineering at USNA. [Annapolis, MD: U.S. Naval Academy, 1996.

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L, Tomsic Joan, Eastlake Charles N, and Society of Automotive Engineers, eds. SAE dictionary of aerospace engineering. 2nd ed. Warrendale, PA: Society of Automotive Engineers, 1998.

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Buttazzo, Giuseppe, and Aldo Frediani. Variational Analysis and Aerospace Engineering. New York, NY: Springer New York, 2009. http://dx.doi.org/10.1007/978-0-387-95857-6.

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Frediani, Aldo, Bijan Mohammadi, Olivier Pironneau, and Vittorio Cipolla, eds. Variational Analysis and Aerospace Engineering. Cham: Springer International Publishing, 2016. http://dx.doi.org/10.1007/978-3-319-45680-5.

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Engineers, Society of Automotive, ed. SAE dictionary of aerospace engineering. Warrendale, PA: Society of Automotive Engineers, 1992.

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le-Yiśraʼel, Ṭekhniyon Makhon ṭekhnologi, ed. Aerospace engineering: Research, 1986-1991. Haifa, Israel: Technion-Israel Institute of Technology, 1991.

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Singh, Sanjay, Perumalla Janaki Ramulu, and Sachin Singh Gautam, eds. Recent Advances in Aerospace Engineering. Singapore: Springer Nature Singapore, 2024. http://dx.doi.org/10.1007/978-981-97-1306-6.

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Book chapters on the topic "Aerospace engineering"

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Shafer, Wade H. "Aerospace Engineering." In Masters Theses in the Pure and Applied Sciences, 1–10. Boston, MA: Springer US, 1996. http://dx.doi.org/10.1007/978-1-4613-0393-0_1.

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Shafer, Wade H. "Aerospace Engineering." In Masters Theses in the Pure and Applied Sciences, 1–9. Boston, MA: Springer US, 1997. http://dx.doi.org/10.1007/978-1-4615-5969-6_1.

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Shafer, Wade H. "Aerospace Engineering." In Masters Theses in the Pure and Applied Sciences, 1–8. Boston, MA: Springer US, 1992. http://dx.doi.org/10.1007/978-1-4615-3412-9_1.

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Shafer, Wade H. "Aerospace Engineering." In Masters Theses in the Pure and Applied Sciences, 1–8. Boston, MA: Springer US, 1992. http://dx.doi.org/10.1007/978-1-4615-3474-7_1.

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Shafer, Wade H. "Aerospace Engineering." In Masters Theses in the Pure and Applied Sciences, 1–10. Boston, MA: Springer US, 1989. http://dx.doi.org/10.1007/978-1-4613-0599-6_1.

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Shafer, Wade H. "Aerospace Engineering." In Masters Theses in the Pure and Applied Sciences, 1–6. Boston, MA: Springer US, 1986. http://dx.doi.org/10.1007/978-1-4684-5197-9_1.

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Shafer, Wade H. "Aerospace Engineering." In Masters Theses in the Pure and Applied Sciences, 1–9. Boston, MA: Springer US, 1993. http://dx.doi.org/10.1007/978-1-4615-2832-6_1.

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Shafer, Wade H. "Aerospace Engineering." In Masters Theses in the Pure and Applied Sciences, 1–7. Boston, MA: Springer US, 1997. http://dx.doi.org/10.1007/978-1-4757-5782-8_1.

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Shafer, Wade H. "Aerospace Engineering." In Masters Theses in the Pure and Applied Sciences, 1–11. Boston, MA: Springer US, 1993. http://dx.doi.org/10.1007/978-1-4615-2453-3_1.

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Shafer, Wade H. "Aerospace Engineering." In Masters Theses in the Pure and Applied Sciences, 1–13. Boston, MA: Springer US, 1994. http://dx.doi.org/10.1007/978-1-4615-1969-0_1.

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Conference papers on the topic "Aerospace engineering"

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Scott, Bruce. "Aerospace Co-Operative Engineering." In International Pacific Air and Space Technology Conference and Exposition. 400 Commonwealth Drive, Warrendale, PA, United States: SAE International, 1987. http://dx.doi.org/10.4271/872463.

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Crawley, Ed, Robert Niewoehner, and Jean Koster. "North American Aerospace Project: CDIO in Aerospace Engineering Education." In 48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition. Reston, Virigina: American Institute of Aeronautics and Astronautics, 2010. http://dx.doi.org/10.2514/6.2010-532.

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Barata, Jorge, Fernando Neves, and Andre Silva. "The History of Aerospace/Aerospace/Aeronautics Engineering in Portugal." In 50th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition. Reston, Virigina: American Institute of Aeronautics and Astronautics, 2012. http://dx.doi.org/10.2514/6.2012-954.

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Koenig, K., L. Hester, and T. Hannigan. "Sports and aerospace engineering education." In 32nd Aerospace Sciences Meeting and Exhibit. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1994. http://dx.doi.org/10.2514/6.1994-855.

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Briggs, Fred C. "Advances in Aerospace Software Engineering." In 2018 AIAA Information Systems-AIAA Infotech @ Aerospace. Reston, Virginia: American Institute of Aeronautics and Astronautics, 2018. http://dx.doi.org/10.2514/6.2018-1983.

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Lohar, Fayyaz. "Aerospace Engineering Program at IIUM." In 42nd AIAA Aerospace Sciences Meeting and Exhibit. Reston, Virigina: American Institute of Aeronautics and Astronautics, 2004. http://dx.doi.org/10.2514/6.2004-420.

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Jacob, J. "Aerospace engineering education in a mechanical engineering environment." In 38th Aerospace Sciences Meeting and Exhibit. Reston, Virigina: American Institute of Aeronautics and Astronautics, 2000. http://dx.doi.org/10.2514/6.2000-527.

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Rock, Nigel. "Automobile/Aerospace Synergy in Engineering Analysis." In Aerospace Atlantic Conference & Exposition. 400 Commonwealth Drive, Warrendale, PA, United States: SAE International, 1991. http://dx.doi.org/10.4271/911121.

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Bridges, David. "Of Aeronautics, Aerophysics, and Aerospace: Aerospace Engineering at Mississippi State University." In 43rd AIAA Aerospace Sciences Meeting and Exhibit. Reston, Virigina: American Institute of Aeronautics and Astronautics, 2005. http://dx.doi.org/10.2514/6.2005-330.

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Prunariu, Dumitru-Dorin. "AEROSPACE ENGINEERING DUES TO GLOBAL SUSTAINABILITY." In 18th International Multidisciplinary Scientific GeoConference SGEM2018. Stef92 Technology, 2018. http://dx.doi.org/10.5593/sgem2018/6.1/s28.068.

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Reports on the topic "Aerospace engineering"

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Kashyap, Nabil. Aerospace Engineering / Chemical Kinetics - University of Michigan. Purdue University Libraries, March 2012. http://dx.doi.org/10.5703/1288284314989.

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Calkins, Dale E., Richard S. Gaevert, Frederick J. Michel, and Karen J. Richter. Aerospace System Unified Life Cycle Engineering Producibility Measurement Issues. Fort Belvoir, VA: Defense Technical Information Center, May 1989. http://dx.doi.org/10.21236/ada210937.

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Cowles, Bradford A., and Daniel Backman. Advancement and Implementation of Integrated Computational Materials Engineering (ICME) for Aerospace Applications. Fort Belvoir, VA: Defense Technical Information Center, March 2010. http://dx.doi.org/10.21236/ada529049.

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Barkan, Terrance. The Role of Graphene in Achieving e-Mobility in Aerospace Applications. 400 Commonwealth Drive, Warrendale, PA, United States: SAE International, December 2022. http://dx.doi.org/10.4271/epr2022030.

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<div class="section abstract"><div class="htmlview paragraph">Advanced two-dimensional (2D) materials discovered in the last two decades are now being produced at scale and are contributing to a wide range of performance enhancements in engineering applications. The most well-known of these novel materials is graphene, a nearly transparent nanomaterial comprising a single layer of bonded carbon atoms. In relative terms, it has the highest level of heat and electrical conductivity, protects against ultraviolet rays, and is strongest material ever measured. These properties have made graphene an attractive potential material for a variety of applications, particularly for transportation related uses, and especially for aerospace engineering. </div><div class="htmlview paragraph"><b>The Role of Graphene in Achieving e-Mobility in Aerospace Applications</b> reviews the current state of graphene-related aerospace applications and identifies the technological challenges facing engineers that look to benefit from graphene’s attractive properties.</div><div class="htmlview paragraph"><a href="https://www.sae.org/publications/edge-research-reports" target="_blank">Click here to access the full SAE EDGE</a><sup>TM</sup><a href="https://www.sae.org/publications/edge-research-reports" target="_blank"> Research Report portfolio.</a></div></div>

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Muelaner, Jody Emlyn. Generative Design in Aerospace and Automotive Structures. 400 Commonwealth Drive, Warrendale, PA, United States: SAE International, July 2024. http://dx.doi.org/10.4271/epr2024016.

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<div class="section abstract"><div class="htmlview paragraph">Semi-automated computational design methods involving physics-based simulation, optimization, machine learning, and generative artificial intelligence (AI) already allow greatly enhanced performance alongside reduced cost in both design and manufacturing. As we progress, developments in user interfaces, AI integration, and automation of workflows will increasingly reduce the human inputs required to achieve this. With this, engineering teams must change their mindset from designing products to specifying requirements, focusing their efforts on testing and analysis to provide accurate specifications.</div><div class="htmlview paragraph"><b>Generative Design in Aerospace and Automotive Structures</b> discusses generative design in its broadest sense, including the challenges and recommendations regarding multi-stage optimizations.</div><div class="htmlview paragraph"><a href="https://www.sae.org/publications/edge-research-reports" target="_blank">Click here to access the full SAE EDGE</a><sup>TM</sup><a href="https://www.sae.org/publications/edge-research-reports" target="_blank"> Research Report portfolio.</a></div></div>

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CALS TEST NETWORK WRIGHT-PATTERSON AFB OH. Engineering Drawing Transfer Using Sundstrand Aerospace, MIL-D-28000A (IGES). Quick Short Test Report. Fort Belvoir, VA: Defense Technical Information Center, November 1992. http://dx.doi.org/10.21236/ada313218.

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Perdigão, Rui A. P. Strengthening Multi-Hazard Resilience with Quantum Aerospace Systems Intelligence. Synergistic Manifolds, January 2024. http://dx.doi.org/10.46337/240301.

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The present work further enhances and deploys our Quantum Aerospace Systems Intelligence technologies (DOI: 10.46337/quasi.230901) onto Multi-Hazard risk assessment and action, from sensing and prediction to modelling, decision support and active response, towards strengthening its fundamental knowledge, awareness and resilience in the face of multi-domain challenges. Moreover, it introduces our updated post-quantum aerospace engineering ecosystem for empowering active system dynamic capabilities to mitigate or even counter multi-hazard threats from space, leveraging our high energy technological physics solutions acting across coevolutionary space-times. These developments are further articulated with our latest Synergistic Nonlinear Quantum Wave Intelligence Networks suite of technologies (DOI: 10.46337/240118), vastly extending the operational capabilities of novel quantum and post-quantum systems to critically adverse thermodynamic conditions e.g. those pertaining situational action across real-world environmental and security theaters of operation.

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AEROSPACE CORP EL SEGUNDO CA. Aerospace Sponsored Research Summary Report for 1 October 1989 Through 30 September 1990. Scientific and Engineering Research. Fort Belvoir, VA: Defense Technical Information Center, December 1990. http://dx.doi.org/10.21236/ada248420.

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McNeil, Linda. Mobile STEMship Discovery Center: K-12 Aerospace-Based Science, Technology, Engineering, and Mathematics (STEM) Mobile Teaching Vehicle. Fort Belvoir, VA: Defense Technical Information Center, August 2015. http://dx.doi.org/10.21236/ada623464.

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Offerdahl, David C. The Defense Acquisition Workforce Improvement Act and Its Impact on the Navy's Aerospace Engineering Duty Officer (AEDO) Community. Fort Belvoir, VA: Defense Technical Information Center, April 1992. http://dx.doi.org/10.21236/ada262000.

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