Investigation of the effect of variable tail dihedral on airplane stability and control-Reference-Cited by-同舟云学术

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Investigation of the effect of variable tail dihedral on airplane stability and control

Published:1988-08-15 Issue: Volume: Page:
ISSN:
Container-title:15th Atmospheric Flight Mechanics Conference
language:
Short-container-title:

Author:

KIDD JAMES¹

Affiliation:

1. USAF, Armament Laboratory, Eglin AFB, FL

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1988-4335

Reference7 articles.

1. 3urhal,Y. Ertugrul. llInvestigation of F-16 Control Failures and Optimal Setting of Functional Controls," MS Thesis, AFIT/GAE/ENG/86D-19. School of Engineering, A i rForce Institute of Technology (AU), Wright Patterson AFB OH,December 1986.

2. ricksenen, Gary E., Vortex Flow Correlation,ll AFWAL-TR-80-3143. A i r Force Wright Aeronautical Laboratories. Wright Patterson AFB OH, pp308-309.

3. , Inc., IMSL User's Manual, Edition 9.2, Houston, TX, 1984.

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1. Effects of Tail Dihedral on Static Stability;Journal of Aircraft;2006-11

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