Author: G. V. BullPublisher:
ISBN:
Category :
Languages : en
Pages : 36
Book Description
Analysis of the Effect of Wing-wing Interference on the Rolling Characteristics of Cruciform Rectangular Wing-body Combinations in Steady Supersonic Flow
Author: G. V. BullApplied Mechanics Reviews
Author: Theoretical Analysis of Total-pressure Loss and Airflow Distribution for Tubular Turbojet Combustors with Constant Annulus and Liner Cross-sectional Areas
Author: A. J. EggersPublisher:
ISBN:
Category : Aerodynamic heating
Languages : en
Pages : 324
Book Description
Scientific and Technical Aerospace Reports
Author: Journal of the Royal Aeronautical Society
Author: Monthly Catalog of United States Government Publications
Author: Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1364
Book Description
Monthly Catalog of United States Government Publications, Cumulative Index
Author: United States. Superintendent of DocumentsPublisher:
ISBN:
Category : United States
Languages : en
Pages : 1366
Book Description
Wing-body Interference at Supersonic Speeds with an Application to Combinations with Rectangular Wings
Author: Jack N. NielsenPublisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 63
Book Description
An exact theoretical method is developed that permits the determination of the pressure field of a wing-body combination having a circular body and wings with supersonic leading and trailing edges. Detailed calculations are performed for the case of a rectangular wing or all-movable control surface on a body at zero angle of attack. Design charts are presented showing the effect of interference on the lift and center-of-pressure position of the wings. The physical basis of the interference is discussed.
Author: 
Author: