Sideslip behavior of elliptic cross-sectional forebodies at high angle of attack

Journal of Aircraft

Volumn 34, Issue 4, 1997, Pages 472-478

  Tajfar, Amir H ^a,b   Lamont, Peter J ^a,b,c  

^a UNIVERSITY OF MANCHESTER   (United Kingdom)

^b Department of Aerospace Engineering ^*  (United Kingdom)

^c AIAA   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT; REYNOLDS NUMBER;

ANGLE OF ATTACK; ELLIPTIC CROSS SECTIONAL FOREBODIES; SIDESLIP BEHAVIOR;

AERODYNAMICS;

EID: 0031190006     PISSN: 00218669     EISSN: 15333868     Source Type: Journal    
DOI: 10.2514/2.2215     Document Type: Article

References (7)

1. Chambers, J. R., Anylin, E. L., and Bowman, J. S., "Effects of a Pointed Nose on Spin Characteristics of Fighter Airplane Models Including Correlation with Theoretical Calculations," NASA TN D-5921, Sept. 1970.
2. Keener, E. R., and Chapman G. T., "Onset of Aerodynamic Side Force at Zero Sideslip on Symmetric Forebodies at High Angles of Attack," AIAA Paper 74-770, Aug. 1974.
3. Coe, P. L., Jr., Chambers, J. R., and Letko, W., "Asymmetric Lateral-Directional Characteristics of Pointed Bodies of Revolution at High Angles of Attack," NASA TN D-7095, Nov. 1972.
4. Lamont, P. J., and Kennaugh, A., "Multiple Solutions for Aircraft Sideslip Behaviour at High Angles of Attack," AIAA Paper 89-0645, Jan. 1989.
5. Lamont, P. J., and Kennaugh, A., "Total Incidence Plane Aerodynamics: The Key to Understanding High Incidence Flight Dynamics," Journal of Aircraft, Vol. 28, No. 7, 1991, pp. 431-435.
6. Grafton, S. B., Groum, M. A., and Nguyen, L. T, "High Angle of Attack Stability Characteristics of Three Surface Fighter Configurations," NASA TM 84584, March 1983.
7. Brandon, J. M., and Nguyen, L. T., "Experimental Study of Effects of Forebody Geometry on High Angle of Attack Static and Dynamic Stability," AIAA Paper 86-0331, Jan. 1986.