Fundamentals of airplane flight mechanics

Fundamentals of Airplane Flight Mechanics

Volumn , Issue , 2007, Pages 1-298

  Hull, David G ^a  

^a UNIVERSITY OF TEXAS AT AUSTIN   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

EID: 84891979758     PISSN: None     EISSN: None     Source Type: Book    
DOI: 10.1007/978-3-540-46573-7     Document Type: Book

References (15)

1. AD Abott, I. H., and von Doenhoff, A. E., Theory of Wing Sections, Dover, New York, 1959.
2. An Anon, U.S. Standard Atmosphere, 1962, U.S. Government Printing Office, Washington, D.C., December 1962.
3. ER Etkin, B., and Reid, L.D., Dynamics of Flight, 3nd Edition, Wiley, New York, 1996.
4. Ga "GASP-General Aviation Synthesis Program, Vol. III, Aerodynamics", NASA CR-152303, January, 1978.
5. Ho Hoak, D.E., USAF Stability and Control Datcom, published in 1960, revised in 1978, available from DARcorporation, Lawrence, Kansas.
6. Hu Hull, D.G., Optimal Control Theory for Applications, Springer, New York, 2003.
7. Mi1 Miele, A., Flight Mechanics, Vol. I, Theory of Flight Paths, Addison-Wesley, Reading MA, 1962.
8. Mi2 Miele, A., Wang, T., and Melvin, W., Optimization and Acceleration Guidance of Flight Trajectories in a Windshear, Journal of Guidance, Control, and Dynamics, Vol. 10, No. 4, July-August pp. 368-377, 1987.
9. Ne Nelson, R.C., Flight Stability and Automatic Control, McGraw-Hill, New York, 1989.
10. Pa Pamadi, B.N., Performance, Stability, Dynamics, and Control of Airplanes, Second Edition, American Institute of Aeronautics and Astronautics, Reston VA, 2004.
11. Pe Perkins, Courtland D. "Development of Airplane Stability and Control Technology", AIAA Journal of Aircraft, Vol. 7, No. 4, July-August, 1970.
12. Ro1 Roskam, J., Methods for Estimating Stability and Control Derivatives of Conventional Subsonic Airplanes, DARcorporation, Lawrence, Kansas, 1971.
13. Ro2 Roskam, J., Flight Dynamics of Rigid and Elastic Airplanes, Vol. 1, DARcorporation, Lawrence, Kansas, 1972.
14. Sc Schemensky, R.T., Development of an Emperically Based Computer Program to Predict the Aerodynamic Characteristics of Aircraft, Volume 1, Empirical Methods, Technical Report AFFDL-TR-73-144, Wright-Patterson Air Force Base, Ohio, November 1973.
15. Ye Yechout, T.R., Introduction to Aircraft Flight Mechanics, American Institute of Aeronautics and Astronautics, Reston VA, 2004.