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

Acta Astronautica

Volumn 4, Issue 1-2, 1977, Pages 99-109

  Jones, Robert T ^a  

^a NASA AMES RESEARCH CENTER   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT - SUPERSONIC SPEEDS;

AERODYNAMICS;

EID: 0017445161     PISSN: 00945765     EISSN: None     Source Type: Journal    
DOI: 10.1016/0094-5765(77)90035-2     Document Type: Article

References (13)

1. Investigation of stability and control characteristics of an airplane model with a skewed wing in the Langley free flight tunnel
2. Transonic equivalence rule: a nonlinear problem involving lift
3. Study of low aspect ratio swept and oblique wings
4. Effect of Krüger nose flaps on the experimental force and moment characteristics of an oblique wing
5. The spanwise distribution of lift for minimum induced drag of wings having a given lift and a given bending moment
6. The minimum drag of thin wings in frictionless flow
7. Theoretical determination of the minimum drag of airfoils at supersonic speeds
8. Aeroelastic stability and control of an oblique wing
9. Study of the single-body yawed-wing aircraft concept
10. Slewed wing supersonics
11. Lift/drag ratios of optimized slewed elliptic wings at supersonic speeds
12. Static aeroelasticity and the flying wing, revisited, Engineering Note