0
RESEARCH PAPERS

Some Stability and Control Aspects of Airframe/Propulsion System Interactions on the YF-12 Airplane

[+] Author and Article Information
D. T. Berry, G. B. Gilyard

Handling Qualities Branch, NASA Flight Research Center, Edwards, Calif.

J. Eng. Ind 96(3), 820-826 (Aug 01, 1974) (7 pages) doi:10.1115/1.3438447 History: Received July 31, 1973; Online July 15, 2010

Abstract

Airframe/propulsion system interactions can strongly affect the stability and control of supersonic cruise aircraft. These interactions generate forces and moments similar in magnitude to those produced by the aerodynamic controls, and can cause significant changes in vehicle damping and static stability. This in turn can lead to large aircraft excursions or high pilot workload, or both. For optimum integration of an airframe and its jet propulsion system, these phenomena may have to be taken into account.

Copyright © 1974 by ASME
Your Session has timed out. Please sign back in to continue.

References

Figures

Tables

Errata

Discussions

Some tools below are only available to our subscribers or users with an online account.

Related Content

Customize your page view by dragging and repositioning the boxes below.

Related Journal Articles
Related eBook Content
Topic Collections

Sorry! You do not have access to this content. For assistance or to subscribe, please contact us:

  • TELEPHONE: 1-800-843-2763 (Toll-free in the USA)
  • EMAIL: asmedigitalcollection@asme.org
Sign In