Extension of the equivalent angle of attack prediction method-Reference-Cited by-同舟云学术

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Extension of the equivalent angle of attack prediction method

Published:1984-01-09 Issue: Volume: Page:
ISSN:
Container-title:22nd Aerospace Sciences Meeting
language:
Short-container-title:

Author:

STOY S.¹,VUKELICH S.¹

Affiliation:

1. McDonnell Douglas Astronautics Co., St.Louis, MO

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1984-311

Reference14 articles.

1. Missile Aerodynamics

2. Hemsch, M. J., Nielsen, J. N., Smith, C, A., and Perkins, 5. C. Jr. "Component Aero 4- namic Characteristics of Banked Crucifor-Ill Missiles with Arbitrary Control Deflections," AlAA Paper 77-1153.

3. Vukelich, S. R."Development Feasihiiiiy of Missile Datcom," AFWAL-TR-81-3130.

Cited by 8 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. Fin dihedral effects on wing-body carryover for supersonic noncircular missiles;Journal of Spacecraft and Rockets;1995-05

2. Wing-body carryover for noncircular missiles;Journal of Spacecraft and Rockets;1995-05

3. Fin-planform effects on lift and center of pressure for supersonic missiles;Journal of Spacecraft and Rockets;1993-11

4. Fin dihedral effects on aerodynamics of supersonic missiles with square and triangular fuselage cross sections;9th Applied Aerodynamics Conference;1991-08-17

5. Wing-body interference lift for supersonic missiles with elliptical cross-section fuselages;Journal of Spacecraft and Rockets;1989-09

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