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Relevant bibliographies by topics / Air Vehicles Directorate

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Academic literature on the topic 'Air Vehicles Directorate'

Author: Grafiati

Published: 4 June 2021

Last updated: 1 February 2022

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Journal articles on the topic "Air Vehicles Directorate"

1

Leak, Chris. "Epilogue to MERIT: Lessons Learned in Developing an Interactive Environmental Database." Journal of the IEST 42, no. 4 (July 14, 1999): 21–28. http://dx.doi.org/10.17764/jiet.42.4.kp2r7pj019u316l7.

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MERIT, Mission Environmental Requirements Integration Technology, is an interactive environmental database developed by the Air Force Wright Laboratory's Flight Dynamics Directorate (currently the Air Vehicles Directorate of the Air Force Research Laboratory). The purpose of this MS Windows-based application is to quickly and accurately estimate, during the early conceptual design stage, the environments to which stores carried externally on fighter/attack aircraft will be exposed throughout all phases of the life cycle (such as manufacturing, deployment, storage, and operational usage). MERIT is currently used at approximately 75 locations within 25 companies and government agencies. During the development of the MERIT system, many important lessons were learned regarding the creation of environmental databases to support materiel acquisition functions (such as design, test, and maintenance). In this paper, the scope and capabilities of MERIT will be described in more detail. The basis for the lessons learned will be explained and illustrated through examples from the system's development history.

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2

Rita, Rita, and Rosita Sinaga. "Evaluasi Pelayanan Kinerja Angkutan Pemadu Moda di Bandara Soekarno Hatta dan Upaya Peningkatannya." Warta Penelitian Perhubungan 23, no. 1 (May 15, 2019): 91. http://dx.doi.org/10.25104/warlit.v23i1.1054.

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Soekarno-Hatta International Airport as a gateway has supported facilities such as the availability of airport transportation service integrator modes, namely: Damri Bus, Taxi, Bus Primajasa, Cipaganti Shuttle, Shuttle Bus, Transport Charter, City transport, and Motor Vehicle/Ojek as an alternative option for passenger air transport to final destination in Soeakrno Hatta Airport. Based SKEP. Adbandara Number ADSH.03/HK.30/III/2000, concerning Rules and Procedures of activities at Soekarno Hatta Airport in Article 78 regarding the operation of public transportation (1) describedthe permission of the operation of public transport in Soekarno Hatta Airport by the Directorate General of Land Transportation. Airline flight schedules both domestic and international flights have been adapted to the schedule of available modes of transport integrator at Soekarno Hatta Airport for passengers who want to use a transportation mode integrator who will travel tmuards the final destination is not too long to wait in the waiting room Soekarno Hatta Airport.Keywords: Service, Performance Feeder Transportation

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3

Lawrence, B., C. R. Theodore, W. Johnson, and T. Berger. "A handling qualities analysis tool for rotorcraft conceptual designs." Aeronautical Journal 122, no. 1252 (May 31, 2018): 960–87. http://dx.doi.org/10.1017/aer.2018.43.

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ABSTRACTOver the past decade, NASA, under a succession of rotary-wing programs, has been moving towards coupling multiple discipline analyses to evaluate rotorcraft conceptual designs. Handling qualities is one of the component analyses to be included in such a future Multidisciplinary Analysis and Optimization framework for conceptual design of Vertical Take-Off and Landing (VTOL) aircraft. Similarly, the future vision for the capability of the Concept Design and Assessment Technology Area of the U.S Army Aviation Development Directorate also includes a handling qualities component. SIMPLI-FLYD is a tool jointly developed by NASA and the U.S. Army to perform modelling and analysis for the assessment of the handling qualities of rotorcraft conceptual designs. Illustrative scenarios of a tiltrotor in forward flight and a single-main rotor helicopter at hover are analysed using a combined process of SIMPLI-FLYD integrated with the conceptual design sizing tool NDARC. The effects of variations of input parameters such as horizontal tail and tail rotor geometry were evaluated in the form of margins to fixed- and rotary-wing handling qualities metrics and the computed vehicle empty weight. The handling qualities Design Margins are shown to vary across the flight envelope due to both changing flight dynamics and control characteristics and changing handling qualities specification requirements. The current SIMPLI-FLYD capability, lessons learned from its use and future developments are discussed.

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4

Lane, Steven A., John Higgins, Adam Biskner, Greg Sanford, Chris Springer, and Jerome Berg. "Out-of-Autoclave Composite Fairing Design, Fabrication, and Test." Journal of Manufacturing Science and Engineering 133, no. 3 (June 1, 2011). http://dx.doi.org/10.1115/1.4004321.

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This paper documents a recent R&D effort conducted by the Air Force Research Laboratory, Space Vehicles Directorate, to assess the feasibility of fabricating large composite launch vehicle fairings without the use of autoclaves. Two composite manufacturing approaches were demonstrated: vacuum-bag compaction with oven cure and vacuum assisted resin transfer molding with oven cure. For this project, a 2.8-m diameter fairing was developed for the Minotaur IV launch system. The prototype fairing was instrumented and tested up to qualification test loads. No damage or permanent deformations were observed. Measured strain and displacement data were compared to model predictions; trends and amplitudes were generally in agreement.

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Books on the topic "Air Vehicles Directorate"

1

Air Force Research Laboratory (Wright-Patterson Air Force Base, Ohio). Air Vehicles Directorate. Air Vehicles Directorate. Wright-Patterson Air Force Base, Ohio: Air Force Research Laboratory, Air Vehicles Directorate, 2004.

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2

Air Force Research Laboratory (Wright-Patterson Air Force Base, Ohio). Air Vehicles Directorate. Air Vehicles Directorate. Wright-Patterson Air Force Base, Ohio: Air Force Research Laboratory, Air Vehicles Directorate, 2004.

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3

Tanner, Patrick J. Vehicle maintenance manpower requirements for U.S. Army Installation Directorates of Engineering and Housing based on Air Force, Navy, and Army reserves' staffing techniques. Champaign, Ill: US Army Corps of Engineers, Construction Engineering Research Laboratory, 1986.

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4

Klein, J. A. P. Luchtverontreiniging, emissies door wegverkeer: Methodiek vastelling emissiefactoren : onderzoek op verzoek van Ministerie van Verkeer en Waterstaat, Directoraat-Generaal Rijkswaterstaat, Dienst Weg- en Waterbouwkunde. 's-Gravenhage: SDU/CBS-Publikaties, 1993.

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5

Technology Selection for the Air Force Research Laboratory Air Vehicles Directorate: An Analysis Using Value Focused Thinking. Storming Media, 1999.

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Conference papers on the topic "Air Vehicles Directorate"

1

Tilmann, Carl, Roger Kimmel, Gregory Addington, and James Myatt. "Flow Control Research and Applications at the AFRL's Air Vehicles Directorate." In 2nd AIAA Flow Control Conference. Reston, Virigina: American Institute of Aeronautics and Astronautics, 2004. http://dx.doi.org/10.2514/6.2004-2622.

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2

Radzykewycz, Dan, Jerry Fausz, and William James. "Energy storage technology development at the Air Force Research Laboratory Space Vehicles Directorate." In Space Technology Conference and Exposition. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1999. http://dx.doi.org/10.2514/6.1999-4503.

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3

Guerrero, Jim, Peter Wegner, Steven Buckley, Brandon Arritt, and Eugene Fosness. "Composite tank development efforts at the Air Force Research Laboratory Space Vehicles Directorate." In AIAA Space 2001 Conference and Exposition. Reston, Virigina: American Institute of Aeronautics and Astronautics, 2001. http://dx.doi.org/10.2514/6.2001-4606.

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4

Buckley, Steven, Eugene Fosness, and Waylon Gammill. "Deployment and release devices efforts at the Air Force Research Laboratory space vehicles directorate." In AIAA Space 2001 Conference and Exposition. Reston, Virigina: American Institute of Aeronautics and Astronautics, 2001. http://dx.doi.org/10.2514/6.2001-4601.

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5

Doyle, Derek, Whitney Reynolds, and Brandon Arritt. "Structural Health Monitoring as an Enabler for Responsive Satellites: An Update." In ASME 2010 Conference on Smart Materials, Adaptive Structures and Intelligent Systems. ASMEDC, 2010. http://dx.doi.org/10.1115/smasis2010-3747.

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The Air Force Research Laboratory/Space Vehicles Directorate (AFRL/RVSV) is developing Structural Health Monitoring (SHM) technologies in support of the Responsive Space (RS) initiative with plans for future capabilities on orbit to assist in overall awareness. Such technologies will significantly reduce the amount of time and effort required to assess a satellite’s structural surety without increasing system level risk associated with changed testing. Furthermore, successful implementation of multifunctional sensor capabilities may lead to savings in size, weight, and power (SWAP) allowing more options for technical performance. Although SHM development efforts abound, RS drives unique requirements on the development of these SHM systems; the biggest difference being that deviation from maintenance requires a technology driver. This paper describes several potential niches for SHM technology development efforts by AFRL, aimed at solving those technical issues unique to responsive space, as well as how an ideal SHM system could be implemented within various other processes including the potential for on-orbit performance.

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6

Binney, David A., Harsh Vinayak, Yuiry Gmirya, Lawrence M. Zunski, D. R. Houser, and E. C. Ames. "Face Gear Transmission Development Program at Sikorsky Aircraft." In ASME 2003 International Design Engineering Technical Conferences and Computers and Information in Engineering Conference. ASMEDC, 2003. http://dx.doi.org/10.1115/detc2003/ptg-48039.

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Sikorsky Aircraft, under a cooperative agreement with AATD (Aviation Applied Technology Directorate), has launched a four-year program, RDS-21 (Rotorcraft Drive Systems for the 21st Century), to develop face gear transmissions. RDS-21 addresses key technologies needed to enhance the drive systems of the objective force aircraft while developing new technologies to support the development of a new face gear drive system for Unmanned Air Vehicles (UAV) and the Future Utility Rotorcraft (FUR). Some of the initial funding for face gear development came from a partnership with Army MANTECH. This paper presents an overview of the RDS-21 face gear program and summarizes major milestones achieved to-date. Sikorsky has pursued face gear technologies by partnering with two key institutions. The GearLab at The Ohio State University has developed face gear analysis and design software while the other partner, Gleason Pfauter Inc., has developed face gear manufacturing technology. The methods developed for the design and analysis of face gears and some of the results of their application are covered in this paper. A mathematical model of the face gear generation process is created. The model facilitates the calculation of quantities of interest such as sliding velocities and contact ratio. Digital master gears are created for inspection purposes. A gear analysis software package is used to compute the loads and stresses in the gears. Work is continuing at The Ohio State University to create proprietary face gear analysis software for Sikorsky that can quickly run many design configurations.

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