X-29 forward swept wing aerodynamic overview-Reference-Cited by-同舟云学术

X-29 forward swept wing aerodynamic overview

Published:1983-07-13 Issue: Volume: Page:
ISSN:
Container-title:Applied Aerodynamics Conference
language:
Short-container-title:

Author:

MOORE M.¹,FREI D.¹

Affiliation:

1. Grumman Aerospace Corp., Bethpage, NY

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1983-1834

Reference6 articles.

1. Wind tunnel investigation of the transonic aerodynamic characteristics of forward swept wings

2. The Forward Swept Wing - A unique design challenge

3. Kauffman, R.C., Scher, S.H.,Cohen, L.E. "Static Aerodynamic Characteristics of a 117 Scale Model of the F-5A Airplane at Angles of Attack from 0 to 90 Degrees & Angles of Sideslipfrom -10 to 30 Degrees for a Mach Number of 0.20,'' NASA TMX-62339, April 1974.

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