Relevant bibliographies by topics / Aerodynamics. Flight. Aerospace engineering

Contents

  1. Journal articles
  2. Dissertations / Theses
  3. Books
  4. Book chapters
  5. Conference papers

Academic literature on the topic 'Aerodynamics. Flight. Aerospace engineering'

Author: Grafiati
Published: 4 June 2021
Last updated: 16 February 2022

Create a spot-on reference in APA, MLA, Chicago, Harvard, and other styles

Select a source type:

Consult the lists of relevant articles, books, theses, conference reports, and other scholarly sources on the topic 'Aerodynamics. Flight. Aerospace engineering.'

Next to every source in the list of references, there is an 'Add to bibliography' button. Press on it, and we will generate automatically the bibliographic reference to the chosen work in the citation style you need: APA, MLA, Harvard, Chicago, Vancouver, etc.

You can also download the full text of the academic publication as pdf and read online its abstract whenever available in the metadata.

Journal articles on the topic "Aerodynamics. Flight. Aerospace engineering"

1

Bangash, Z. A., R. P. Sanchez, A. Ahmed, and M. J. Khan. "Aerodynamics of Formation Flight." Journal of Aircraft 43, no. 4 (2006): 907–12. http://dx.doi.org/10.2514/1.13872.

Full text
APA, Harvard, Vancouver, ISO, and other styles
2

Zhang, Jing, Wenwen Kang, and Lingyu Yang. "Aerodynamic benefits of boundary layer ingestion for distributed propulsion configuration." Aircraft Engineering and Aerospace Technology 91, no. 10 (2019): 1285–94. http://dx.doi.org/10.1108/aeat-06-2018-0174.

Full text
Abstract:
Purpose Boundary layer ingestion (BLI) is one of the probable noteworthy features of distributed propulsion configuration (DPC). Because of BLI, strong coupling effects are generated between the aerodynamics and propulsion system of aircraft, leading to the specific lift and drag aerodynamic characteristics. This paper aims to propose a model-based comprehensive analysis method to investigate this unique aerodynamic. Design/methodology/approach To investigate this unique aerodynamics, a model-based comprehensive analysis method is proposed. This method uses a detailed mathematical model of the
APA, Harvard, Vancouver, ISO, and other styles
3

Ghommem, M., and V. M. Calo. "Flapping wings in line formation flight: a computational analysis." Aeronautical Journal 118, no. 1203 (2014): 485–501. http://dx.doi.org/10.1017/s0001924000009325.

Full text
Abstract:
AbstractThe current understanding of the aerodynamics of birds in formation flights is mostly based on field observations. The interpretation of these observations is usually made using simplified aerodynamic models. Here, we investigate the aerodynamic aspects of formation flights. We use a potential flow solver based on the unsteady vortex lattice method (UVLM) to simulate the flow over flapping wings flying in grouping arrangements and in proximity of each other. UVLM has the capability to capture unsteady effects associated with the wake. We demonstrate the importance of properly capturing
APA, Harvard, Vancouver, ISO, and other styles
4

Stollery, J. L. "Aerodynamics, Aeronautics and Flight Mechanics." Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering 211, no. 1 (1997): 63–64. http://dx.doi.org/10.1177/095441009721100102.

Full text
APA, Harvard, Vancouver, ISO, and other styles
5

Prothin, S., C. Fernandez Escudero, N. Doué, and T. Jardin. "Aerodynamics of MAV rotors in ground and corner effect." International Journal of Micro Air Vehicles 11 (January 2019): 175682931986159. http://dx.doi.org/10.1177/1756829319861596.

Full text
Abstract:
The work presented in this paper is part of a project called ARChEaN (Aerodynamic of Rotors in Confined ENvironment) whose objective is to study the interactions of a micro drone rotor with its surroundings in the case of flight in enclosed environments such as those encountered, for example, in archeological exploration of caves. To do so the influence of the environment (walls, ground, ceiling, etc) on the rotor’s aerodynamic performance as well as on the flow field between the rotor and the surroundings is studied. This paper focuses on two different configurations, flight near the ground a
APA, Harvard, Vancouver, ISO, and other styles
6

Gennaretti, M., and G. Bernardini. "Aeroelastic response of helicopter rotors using a 3D unsteady aerodynamic solver." Aeronautical Journal 110, no. 1114 (2006): 793–801. http://dx.doi.org/10.1017/s0001924000001664.

Full text
Abstract:
The prediction of blade deflections and vibratory hub loads concerning helicopter main rotors in forward flight is the objective of this work. They are determined by using an aeroelastic model derived through the coupling between a nonlinear blade structural model and a boundary integral equation solver for three-dimensional, unsteady, potential aerodynamics. The Galerkin method is used for the spatial integration, whereas the periodic blade response is determined by a harmonic balance approach. This aeroelastic model yields a unified approach for aeroelastic response and blade pressure predic
APA, Harvard, Vancouver, ISO, and other styles
7

Kulhánek, Robert. "Identification of a degradation of aerodynamic characteristics of a paraglider due to its flexibility from flight test." Aircraft Engineering and Aerospace Technology 91, no. 6 (2019): 873–79. http://dx.doi.org/10.1108/aeat-06-2018-0162.

Full text
Abstract:
Purpose Aerodynamics of paragliders is very complicated aeroelastic phenomena. The purpose of this work is to quantify the amount of aerodynamic drag related to the flexible nature of a paraglider wing. Design/methodology/approach The laboratory testing on scaled models can be very difficult because of problems in the elastic similitude of such a structure. Testing of full-scale models in a large facility with a large full-scale test section is very expensive. The degradation of aerodynamic characteristics is evaluated from flight tests of the paraglider speed polar. All aspects of the identif
APA, Harvard, Vancouver, ISO, and other styles
8

Escobar-Ruiz, Alan G., Omar Lopez-Botello, Luis Reyes-Osorio, Patricia Zambrano-Robledo, Luis Amezquita-Brooks, and Octavio Garcia-Salazar. "Conceptual Design of an Unmanned Fixed-Wing Aerial Vehicle Based on Alternative Energy." International Journal of Aerospace Engineering 2019 (November 14, 2019): 1–13. http://dx.doi.org/10.1155/2019/8104927.

Full text
Abstract:
This paper focuses on the aerodynamics and design of an unmanned aerial vehicle (UAV) based on solar cells as a main power source. The procedure includes three phases: the conceptual design, preliminary design, and a computational fluid dynamics analysis of the vehicle. One of the main disadvantages of an electric UAV is the flight time; in this sense, the challenge is to create an aerodynamic design that can increase the endurance of the UAV. In this research, the flight mission starts with the attempt of the vehicle design to get at the maximum altitude; then, the UAV starts to glide and bat
APA, Harvard, Vancouver, ISO, and other styles
9

Liu, Haojie, and Yonghui Zhao. "Efficient Training Data Generation for Reduced-Order Modeling in a Transonic Flight Regime." International Journal of Aerospace Engineering 2018 (September 12, 2018): 1–12. http://dx.doi.org/10.1155/2018/4083538.

Full text
Abstract:
In this study, a time-dependent surrogate approach is presented to generate the training data for identifying the reduced-order model of an unsteady aerodynamic system with the variation of mean angle of attack and Mach number in a transonic flight regime. For such a purpose, a finite set of flight samples are selected to cover the flight range of concern at first. Subsequently, the unsteady aerodynamic outputs of the system under given inputs of filtered white Gaussian noise at these flight samples are simulated via CFD technique which solves Euler equations. The unsteady aerodynamic outputs,
APA, Harvard, Vancouver, ISO, and other styles
10

Zyl, L. H. van. "2D and 3D low frequency aerodynamics." Aeronautical Journal 112, no. 1136 (2008): 609–12. http://dx.doi.org/10.1017/s0001924000002578.

Full text
Abstract:
Abstract Unsteady aerodynamic loads on aircraft configurations are used for aeroelastic or flight dynamic analyses. The sources for deriving these loads include strip theory aerodynamics and three-dimensional panel methods. In some applications the behaviour of the unsteady air loads as the frequency approaches zero is important, and it is well known that the behaviour of strip theory aerodynamics employing the exact circulation function differs qualitatively from that of the three-dimensional panel methods such as the subsonic doublet lattice method (DLM). Theoretical results from an earlier
APA, Harvard, Vancouver, ISO, and other styles
More sources

Dissertations / Theses on the topic "Aerodynamics. Flight. Aerospace engineering"

1

Salmons, James Dale. "Developmental flight testing of a half scale unmanned air vehicle." Thesis, Monterey, California : Naval Postgraduate School, 1990. http://handle.dtic.mil/100.2/ADA240347.

Full text
Abstract:
Thesis (M.S. in Aeronautical Engineering)--Naval Postgraduate School, September 1990.<br>Thesis Advisor(s): Howard, Richard M. Second Reader: Pagenkopf, Eric L. "September 1990." Description based on title screen as viewed on December 18, 2009. DTIC Descriptor(s): Unmanned, Flight Testing, Angles, Steady State, Measurement, Vibration, Maneuverability, Marine Corps, Aircraft, Scale Models, Structural Properties, Tail Assemblies, Theses, Angle Of Attack, Estimates, Fuels, Endurance(General), Flight, Response, Scale, Weight, Airframes, Airspeed, Instrumentation, Recording Systems, Sideslip, Mane
APA, Harvard, Vancouver, ISO, and other styles
2

Rhoades, Mark M. "A study of the airwake aerodynamics over the flight deck of an AOR model ship." Monterey, California : Naval Postgraduate School, 1990. http://handle.dtic.mil/100.2/ADA241008.

Full text
Abstract:
Thesis (M.S. in Aeronautical Engineering)--Naval Postgraduate School, September 1990.<br>Thesis Advisor(s): Healey, J. Val. Second Reader: Schmidt, L. V. "September 1990." Description based on title screen as viewed on December 18, 2009. DTIC Descriptor(s): Velocity, Air Flow, Flight Decks, Shear Properties, Measurement, Position(Location), Ships, Models, Layers, Edges, Boundary Layer, Flow Visualization, Tunnels, Curvature, Smoke, Stationary, Bubbles, Patterns, Helium, Flow, Ship Models, Video Signals, Anemometers, Earth Atmosphere, Deflectors, Photographic Equipment. DTIC Identifier(s): Wake
APA, Harvard, Vancouver, ISO, and other styles
3

Eddy, Andito Donisha. "AN INVESTIGATION INTO DELTA WING AERODYNAMICS WITH APPLICATION TO UNMANNED AIRCRAFT IN HIGH ALTITUDE FLIGHT." The Ohio State University, 2018. http://rave.ohiolink.edu/etdc/view?acc_num=osu1532037956695845.

Full text
APA, Harvard, Vancouver, ISO, and other styles
4

Thamann, Michael. "AERODYNAMICS AND CONTROL OF A DEPLOYABLE WING UAV FOR AUTONOMOUS FLIGHT." UKnowledge, 2012. http://uknowledge.uky.edu/me_etds/18.

Full text
Abstract:
UAV development and usage has increased dramatically in the last 15 years. In this time frame the potential has been realized for deployable UAVs to the extent that a new class of UAV was defined for these systems. Inflatable wing UAVs provide a unique solution for deployable UAVs because they are highly packable (some collapsing to 5-10% of their deployed volume) and have the potential for the incorporation of wing shaping. In this thesis, aerodynamic coefficients and aileron effectiveness were derived from the equations of motion of aircraft as necessary parameters for autonomous flight. A w
APA, Harvard, Vancouver, ISO, and other styles
5

Hooper, Jack Charles. "Vertical landing flight envelope definition." Thesis, Luleå tekniska universitet, Rymdteknik, 2020. http://urn.kb.se/resolve?urn=urn:nbn:se:ltu:diva-80717.

Full text
Abstract:
This paper will investigate the development of a landing footprint for a re-entry vehicle. Vehicles can re-enter the atmosphere with a range of orientations, velocities and flight path angles. The central question is whether a vehicle with any combination of these states can be brought to an acceptable landing condition at a particular landing site and with a particular landing speed. To aide in this investigation several models must be implemented, including that of the atmosphere, the vehicles, the Earth, and the aerodynamics. A detailed analysis of the aerodynamic model will be treated, and
APA, Harvard, Vancouver, ISO, and other styles
6

Sebastian, Thomas Jr. "Methods for the Determination of Aerodynamic Parameters and Trajectory Reconstruction of the Orion Command Module from Scale Model Aeroballistic Flight Data." NCSU, 2008. http://www.lib.ncsu.edu/theses/available/etd-11042008-170009/.

Full text
Abstract:
Determination of aerodynamic coeffcients and stability derivatives is necessary in defning a model of the Orion CEV dynamics. This involves reducing experimental data, which can include acceleration, angular rate, or orientation data. This sort of extraction of dynamics from experimental data is often performed on data gathered from experiments conducted on uninstrumented models at indoor ballistics ranges. The US Army Research Laboratory (ARL) has developed a high-g survivable stand-alone instrumentation package that can transmit in-flight measurements of acceleration, angular rate, and local
APA, Harvard, Vancouver, ISO, and other styles
7

Belfield, Eric. "Assessment of Asymmetric Flight on Solar UAS." DigitalCommons@CalPoly, 2016. https://digitalcommons.calpoly.edu/theses/1676.

Full text
Abstract:
An investigation was conducted into the feasibility of using an unconventional flight technique, asymmetric flight, to improve overall efficiency of solar aircraft. In this study, asymmetric flight is defined as steady level flight in a non-wings-level state in- tended to improve solar incidence angle. By manipulating aircraft orientation through roll angle, solar energy collection is improved but aerodynamic efficiency is worsened due to the introduction of additional trim drag. A point performance model was devel- oped to investigate the trade-off between improvement in solar energy collecti
APA, Harvard, Vancouver, ISO, and other styles
8

Gai, Kuo. "Wing Damage Effect on Dragonfly’s Aerodynamic Performance during Takeoff." Wright State University / OhioLINK, 2013. http://rave.ohiolink.edu/etdc/view?acc_num=wright1367934121.

Full text
APA, Harvard, Vancouver, ISO, and other styles
9

Jacobsson, David. "Learning to Fly: Upgraded Aerodynamics and Control Surfaces." Thesis, KTH, Flygdynamik, 2021. http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-299417.

Full text
Abstract:
In recent times the unmanned quadcopter aircraft has been used for a widening range of applications, but for longer distances it still falls short of conventional airplanes in terms of energy usage. There exists hybrid configurations of unmanned aircraft which combine the mobility of quadcopters and the range of fixed-wing aircraft. The transition between the hovering mode and the gliding mode, however, is a complex non-linear control problem. To solve this a recent study applied a neural network as a closed loop controller. This controller was capable of seamless mode transition and could be
APA, Harvard, Vancouver, ISO, and other styles
10

Arustei, Adrian. "Development of a System Identification Tool for Subscale Flight Testing." Thesis, Linköpings universitet, Fluida och mekatroniska system, 2019. http://urn.kb.se/resolve?urn=urn:nbn:se:liu:diva-157292.

Full text
Abstract:
Aircraft system identification has been widely used to this day in applications like control law design, building simulators or extending flight envelopes. It can also be utilized for determining flight-mechanical characteristics in the preliminary design phase of a flight vehicle. In this thesis, three common time-domain methods were implemented in MATLAB for determining the aerodynamic derivatives of a subscale aircraft. For parameter estimation, the equation-error method is quick, robust and can provide good parameter estimates on its own. The output-error method is computationally intensiv
APA, Harvard, Vancouver, ISO, and other styles
More sources

Books on the topic "Aerodynamics. Flight. Aerospace engineering"

1

Greatrix, David R. Powered Flight: The Engineering of Aerospace Propulsion. Springer London, 2012.

Find full text
APA, Harvard, Vancouver, ISO, and other styles
2

Kantha, Lakshmi. Migration on Wings: Aerodynamics and Energetics. Springer Berlin Heidelberg, 2012.

Find full text
APA, Harvard, Vancouver, ISO, and other styles
3

Kroll, Norbert. Computational Flight Testing: Results of the Closing Symposium of the German Research Initiative ComFliTe, Braunschweig, Germany, June 11th-12th, 2012. Springer Berlin Heidelberg, 2013.

Find full text
APA, Harvard, Vancouver, ISO, and other styles
4

K, Remple Robert, ed. Aircraft and rotorcraft system identification: Engineering methods with flight-test examples aircraft and rotorcraft system identification engineering methods with flight-test examples. American Institute of Aeronautics and Astronautics, 2006.

Find full text
APA, Harvard, Vancouver, ISO, and other styles
5

International Congress on Instrumentation in Aerospace Simulation Facilities (16th 1995 Wright-Patterson AFB, Ohio). ICIASF '95 record: International Congress on Instrumentation in Aerospace Simulation Facilities, United States Air Force, Wright Laboratory, Flight Dynamics Directorate, Wright-Patterson AFB, Ohio, USA, July 18-21, 1995. Institute of Electrical and Electronics Engineers, 1995.

Find full text
APA, Harvard, Vancouver, ISO, and other styles
6

Engineering analysis of flight vehicles. Dover, 1992.

Find full text
APA, Harvard, Vancouver, ISO, and other styles
7

International Symposium on Applied Aerodynamics and Design of Aerospace Vehicles (3rd 2007 Trivandrum, India). Recent trends in applied aerodynamics and design: Proceedings of SAROD-2007, November 2007, Thiruvananthapuram, India. Edited by Koner D, Aeronautical Development Agency (India), Indian Space Research Organisation, and Defence Research and Development Laboratory (India). Macmillan India, 2007.

Find full text
APA, Harvard, Vancouver, ISO, and other styles
8

Hyde, Richard Alden. H ∞%x; Aerospace Control Design: A VSTOL Flight Application. Springer London, 1995.

Find full text
APA, Harvard, Vancouver, ISO, and other styles
9

Valasek, John. Morphing aerospace vehicles and structures. John Wiley & Sons, 2012.

Find full text
APA, Harvard, Vancouver, ISO, and other styles
10

American Institute of Aeronautics and Astronautics, ed. Morphing aerospace vehicles and structures. John Wiley & Sons, 2012.

Find full text
APA, Harvard, Vancouver, ISO, and other styles
More sources

Book chapters on the topic "Aerodynamics. Flight. Aerospace engineering"

1

Rizzo, Emanuele, and Aldo Frediani. "Application of Optimisation Algorithms to Aircraft Aerodynamics." In Variational Analysis and Aerospace Engineering. Springer New York, 2009. http://dx.doi.org/10.1007/978-0-387-95857-6_23.

Full text
APA, Harvard, Vancouver, ISO, and other styles
2

Ardema, Mark D., and Bryan C. Asuncion. "Flight Path Optimization at Constant Altitude." In Variational Analysis and Aerospace Engineering. Springer New York, 2009. http://dx.doi.org/10.1007/978-0-387-95857-6_2.

Full text
APA, Harvard, Vancouver, ISO, and other styles
3

Calise, A. J. "Singular Perturbations in Flight Mechanics." In Applied Mathematics in Aerospace Science and Engineering. Springer US, 1994. http://dx.doi.org/10.1007/978-1-4757-9259-1_7.

Full text
APA, Harvard, Vancouver, ISO, and other styles
4

Santini, P. "Stability Problems in Space Flight Mechanics." In Applied Mathematics in Aerospace Science and Engineering. Springer US, 1994. http://dx.doi.org/10.1007/978-1-4757-9259-1_13.

Full text
APA, Harvard, Vancouver, ISO, and other styles
5

Morino, L. "Toward a Unification of Potential and Viscous Aerodynamics: Boundary Integral Formulation." In Applied Mathematics in Aerospace Science and Engineering. Springer US, 1994. http://dx.doi.org/10.1007/978-1-4757-9259-1_5.

Full text
APA, Harvard, Vancouver, ISO, and other styles
6

Arizmendi, B., M. Morelli, G. Parma, M. Zocca, G. Quaranta, and A. Guardone. "In-flight Icing: Modeling, Prediction, and Uncertainty." In Optimization Under Uncertainty with Applications to Aerospace Engineering. Springer International Publishing, 2020. http://dx.doi.org/10.1007/978-3-030-60166-9_15.

Full text
APA, Harvard, Vancouver, ISO, and other styles
7

Cercignani, C. "Mathematical Problems in the Gas Dynamics of High-Altitude Flight." In Applied Mathematics in Aerospace Science and Engineering. Springer US, 1994. http://dx.doi.org/10.1007/978-1-4757-9259-1_4.

Full text
APA, Harvard, Vancouver, ISO, and other styles
8

Sabater, Christian. "Best Practices for Surrogate Based Uncertainty Quantification in Aerodynamics and Application to Robust Shape Optimization." In Optimization Under Uncertainty with Applications to Aerospace Engineering. Springer International Publishing, 2020. http://dx.doi.org/10.1007/978-3-030-60166-9_14.

Full text
APA, Harvard, Vancouver, ISO, and other styles
9

Liu, Hao, Xiaolan Wang, Toshiyuki Nakata, and Kazuyuki Yoshida. "Aerodynamics and Flight Stability of Bio-inspired, Flapping-Wing Micro Air Vehicles." In Intelligent Systems, Control and Automation: Science and Engineering. Springer Japan, 2013. http://dx.doi.org/10.1007/978-4-431-54276-6_10.

Full text
APA, Harvard, Vancouver, ISO, and other styles
10

Laxman, R., Arnab Maity, G. Mallikarjun Rao, and R. Kranthi Kumar. "Optimal Nonlinear Dynamic Inversion-Based Flight Control System Design for an Aerospace Vehicle." In Lecture Notes in Mechanical Engineering. Springer Singapore, 2020. http://dx.doi.org/10.1007/978-981-15-1724-2_8.

Full text
APA, Harvard, Vancouver, ISO, and other styles

Conference papers on the topic "Aerodynamics. Flight. Aerospace engineering"

1

Cochrane, Alexander P., Craig G. Merrett, and Harry H. Hilton. "The influence of time dependent flight and maneuver velocities and elastic or viscoelastic flexibilities on aerodynamic and stability derivatives." In 10TH INTERNATIONAL CONFERENCE ON MATHEMATICAL PROBLEMS IN ENGINEERING, AEROSPACE AND SCIENCES: ICNPAA 2014. AIP Publishing LLC, 2014. http://dx.doi.org/10.1063/1.4904605.

Full text
APA, Harvard, Vancouver, ISO, and other styles
2

Bangash, Zafar, Robin Sanchez, Anwar Ahmed, and M. Khan. "Aerodynamics of Formation Flight." In 42nd AIAA Aerospace Sciences Meeting and Exhibit. American Institute of Aeronautics and Astronautics, 2004. http://dx.doi.org/10.2514/6.2004-725.

Full text
APA, Harvard, Vancouver, ISO, and other styles
3

Lee, Yang Ji, Sang Hun Kang, and Soo Seok Yang. "Study for Starting Characteristics of Scramjet Engine Test Facility (SETF)." In ASME 2012 International Mechanical Engineering Congress and Exposition. American Society of Mechanical Engineers, 2012. http://dx.doi.org/10.1115/imece2012-87193.

Full text
Abstract:
Korea Aerospace Research Institute started on design and development of a hypersonic air-breathing engine test facility from 2000 and completed the test facility installation in July 2009. This facility, designated as the Scramjet engine test facility (SETF), is a blow-down type high enthalpy wind tunnel which has a pressurized air supply system, air heater system, free-jet type test chamber, fuel supply system, facility control/measurement system, and exhaust system with an air ejection. Unlike most aerodynamic wind-tunnel, SETF should simulate the enthalpy condition at a flight condition. To
APA, Harvard, Vancouver, ISO, and other styles
4

Warrick, Doug, Bret Tobalske, Donald Powers, and Michael Dickinson. "The Aerodynamics of Hummingbird Flight." In 45th AIAA Aerospace Sciences Meeting and Exhibit. American Institute of Aeronautics and Astronautics, 2007. http://dx.doi.org/10.2514/6.2007-41.

Full text
APA, Harvard, Vancouver, ISO, and other styles
5

Strganac, Thomas, John Junkins, J. Ko, and Andrew J. Kurdila. "Nonlinear Control Methods for High Energy Limit Cycle Oscillations." In ASME 1999 Design Engineering Technical Conferences. American Society of Mechanical Engineers, 1999. http://dx.doi.org/10.1115/detc99/vib-8385.

Full text
Abstract:
Abstract Limit cycle oscillations, as they manifest in high performance fighter aircraft, remain an area of scrutiny by the aerospace industry and military. Tools for the simulation and prediction of the onset for limit cycle oscillations have matured significantly over the years. Suprisingly, less progress has been made in the derivation of active control methodologies for these inherently nonlinear dynamic phenomena. Even in the cases where it is known that limit cycle oscillation may be observed in particular flight regimes, and active control methodologies are employed to attenuate respons
APA, Harvard, Vancouver, ISO, and other styles
6

Kiefer, Renaud, Marc Vedrines, and Franc¸ois Kiefer. "Complete Design of a VTOL UAV by a Large Group of Students." In ASME 2008 International Mechanical Engineering Congress and Exposition. ASMEDC, 2008. http://dx.doi.org/10.1115/imece2008-67885.

Full text
Abstract:
This paper deals with the complete design and implementation of a small unmanned air vehicle (UAV) in the framework of a project course for engineers. This project takes place within an international contest organised by the french defence and aerospace agency. The objective is to design an autonomous air vehicle that will be able to be operated by soldiers on the battlefield, with embedded sensors and camera, which will be able to explore an urban environment, and detect targets or threads such as snipers. Our team won the first edition of the contest two year ago and is again selected with e
APA, Harvard, Vancouver, ISO, and other styles
7

GAD-EL-HAK, M., and C. M. HO. "Aerodynamics of a missile in unsteady flight." In 24th Aerospace Sciences Meeting. American Institute of Aeronautics and Astronautics, 1986. http://dx.doi.org/10.2514/6.1986-572.

Full text
APA, Harvard, Vancouver, ISO, and other styles
8

Bernal, Luis P., and Huai-Te Yu. "Unsteady Aerodynamics of Low Reynolds Number Flight." In 53rd AIAA Aerospace Sciences Meeting. American Institute of Aeronautics and Astronautics, 2015. http://dx.doi.org/10.2514/6.2015-0038.

Full text
APA, Harvard, Vancouver, ISO, and other styles
9

JUMPER, E., and J. BAUGHN. "The use of Microsoft Flight Simulator in aerospace education." In 9th Applied Aerodynamics Conference. American Institute of Aeronautics and Astronautics, 1991. http://dx.doi.org/10.2514/6.1991-3314.

Full text
APA, Harvard, Vancouver, ISO, and other styles
10

Slingerland, Ronald, Joris Melkert, and D. M. Paassen. "Flight testing as an enhancement of understanding aerodynamics and flight mechanics." In 43rd AIAA Aerospace Sciences Meeting and Exhibit. American Institute of Aeronautics and Astronautics, 2005. http://dx.doi.org/10.2514/6.2005-1074.

Full text
APA, Harvard, Vancouver, ISO, and other styles
You might also be interested in the extended bibliographies on the topic 'Aerodynamics. Flight. Aerospace engineering' for particular source types:
Journal articles Dissertations / Theses Books
We offer discounts on all premium plans for authors whose works are included in thematic literature selections. Contact us to get a unique promo code!

To the bibliography