Flight-Test-Determined Aerodynamic Force and Moment Characteristics of the X-43A at Mach 7.0

Author:

Davis Mark1,White John1

Affiliation:

1. NASA Dryden Flight Research Center

Publisher

American Institute of Aeronautics and Astronautics

Reference12 articles.

1. Hunt, J. L., and Eiswirth,E. A. "NASA'sDual-FuelAirbreathing HypersonicVehicleStudy,"AIAA-96-4591,1996.

2. Marshall, L. A., Corpening, G. P., and Sherrill, R., A Chief Engineer's View of the NASA X-43A Scramjet Flight Test, NASA/TM-2005-212867,2005.

3. Freeman, D. C., Jr., Reubush, D. E., McClinton, C. R., Rausch, V. L., and Crawford, J. L., The NASA Hyper-X Program, NASA TM-1997-207243,1997.

4. Sim, A. G., Flight-Determined Stability and Control Characteristics of the M2-F3 Lifting Body Vehicle, NASA TN D-7511,1973.

5. Iliff, K. W., and Shafer, M. F., Extraction ofStability and ControlDerivativesFrom Orbiter FlightData, NASA Technical Memorandum4500,1993.

Cited by 1 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献

1. The X-43A Six Degree of Freedom Monte Carlo Analysis;46th AIAA Aerospace Sciences Meeting and Exhibit;2008-01-07

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