This content is not included in
your SAE MOBILUS subscription, or you are not logged in.
Aircraft Manoeuvres Simulation Steady and Unsteady Aerodynamic
Technical Paper
2003-01-3034
ISSN: 0148-7191, e-ISSN: 2688-3627
Annotation ability available
Sector:
Language:
English
Abstract
The current work present a simple model to integrate non-linear aerodynamic in conceptual design phase, before wind tunnel testing. A presentation of a simple pitch up maneuver based on three different aerodynamic models is simulated. The simulation indicates different behaviors depending on the aerodynamic model, and shows the importance of including unsteady aerodynamic.
Authors
Citation
Jouannet, C. and Krus, P., "Aircraft Manoeuvres Simulation Steady and Unsteady Aerodynamic," SAE Technical Paper 2003-01-3034, 2003, https://doi.org/10.4271/2003-01-3034.Also In
References
- Shah, Gautam H. “Wind Tunnel Investigation of Aerodynamic and Tail Buffet Characteristics of Leading edge Extension Modifications to the F/A-18,” AIAA-91-2889. Presented at AIAA Atmospheric Flight Mechanics Conference New Orleans, LA Aug. 1991
- Tavoularis, S. Marineau-Mes, S. Woronko, A. Lee, B.H.K. “Tail Buffet of F/A-18 at High Incidence with Sideslip and Roll (Part 1 and 2)” Journal of Aircraft Vol. 38 N.l Jan.–Feb. 2001
- Ericsson, Lars E. “Separated Flow Mechanism in F-18 Wing Rock,” Journal of Aircraft Vol. 33 No. 1 1996
- Erickson Gary E. “Flow Studies of Slender Wing Vortices,” AIAA-80-1423
- Lawford J. A. Beauchamp A. R. “Low-Speed Wind-Tunnel Measurements on a Thin Sharp-Edged Delta Wing with 70° Leading Edge Sweep, with Particular Reference to the Position of Leading-Edge-Vortex Breakdown,” ARC 3338 1963
- Jones, R. T. “Properties of Low Aspect Ratio Wings at Speeds Below and Above the Speed of Sound,” NACA Rept. 835 1946 59 63
- Wentz, W. H., Jr Kohlman D. L. “Wind Tunnel Investigation of Vortex Breakdown on Slender Sharp-Edged Wings,” NASA Research Grant NGR-17-002-043 1968
- Jobe, C. E. “Vortex Breakdown Location over 65 degree Delta Wings Empiricism and Experiment” AIAA-98-2526 1998
- Pelletier, A. Nelson, R. C “An Experimental Study of Static and Dynamic Vortex Breakdown on Slender Delta Wing Planforms,” AIAA-94-1879-CP 1994
- Ericsson, L. E. “Vortex Breakdown Dynamics on Pitching Delta Wings,” AIAA-95-1777-CP 1995
- Soltani, M. R Bragg, M. B. Brandon, J. M. “Experimental Measurement on an Oscillating 70-degree Delta Wing in Subsonic Flow,” AIAA-88-2576-CP 1998
- Polhamus E. C “A Concept of the Vortex Lift of Sharp-Edge Delta Wings Based on Leading-Edge Suction Analogy,” NASA TN D-3767 1966
- Goman, M. G. Khrabov A. N. “State-Space Representation of Aerodynamic Characteristics of an Aircraft at High Angles of Attack,” Journal of Aircraft Vol. 31 No. 5 Sept–Oct. 1994 1109 1115
- Jouannet, C. Krus, P. “Lift Coefficient Predictions for Delta Wings Undergoing Pitching Motions” AIAA 2002-2969, 32 nd AIAA Fluid Dynamic Conference June 2002 St Louis, USA
- Jouannet, C Krus, P “Modeling of Unsteady Aerodynamic Characteristcs of delta wings,” ICAS 2002 Spetembre 2002 Toronto, Canada
- Stevens, B.L. Lewis, F.L. “Aircraft Control and Simulation” 0-471-61397-5 Wiley-Interscience Publication 1992
- Etkin, B. “Dynamic of Atmospheric Flight” 0-471-24620-4 John Wiley & sons 1972
- Lin, G. Lan, C.E. Brandon, J. M. “A Generalized Dynamic Aerodynamic Coefficient Model For Flight Dynamic Applications” AIAA-97-3643
- Reisenthel, P. H. “Development of a Nonlinear Indicial Model for Maneuvring Fighter Aircraft” AIAA-96-0896
- Kolano, E. “Flying the Flanker” www.flightjournal.com