The oblique wing—aircraft design for transonic and low supersonic speeds-Reference-Cited by-同舟云学术

The oblique wing—aircraft design for transonic and low supersonic speeds

Published:1977-01 Issue:1-2 Volume:4 Page:99-109
ISSN:0094-5765
Container-title:Acta Astronautica
language:en
Short-container-title:Acta Astronautica

Author:

Jones Robert T.

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference13 articles.

1. Investigation of stability and control characteristics of an airplane model with a skewed wing in the Langley free flight tunnel;Campbell;NACA Technical Note No. 1208,1947

2. Transonic equivalence rule: a nonlinear problem involving lift;Cheng;J. Fluid Mech.,1975

3. Linearized supersonic flow thesis;Hayes,1968

4. Study of low aspect ratio swept and oblique wings;Hopkins;J. Aircraft,1975

5. Effect of Krüger nose flaps on the experimental force and moment characteristics of an oblique wing;Hopkins;NASA TM X-3372,1976

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