Author: R. C. MEYERPublisher:
ISBN:
Category :
Languages : en
Pages : 1
Book Description
Favorable Wing-body Interference for Aircraft at Supersonic Speed: an Analytic Study of Design Parameters
Scientific and Technical Aerospace Reports
Author: U.S. Government Research Reports
Author: Keywords Index to U.S. Government Technical Reports
Author: Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 88
Book Description
An Integrated Approach to the Analysis and Design of Wings and Wing-body Combinations in Supersonic Flow
Author: Ralph L. CarmichaelPublisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 18
Book Description
Keywords Index to U.S. Government Technical Reports (permuted Title Index).
Author: United States. Department of Commerce. Office of Technical ServicesPublisher:
ISBN:
Category : Government publications
Languages : en
Pages : 618
Book Description
Favorable Interference of Optimized Wing-body Combination with Inlets at Supersonic Speed
Author: T. M. PrituloNASA Technical Memorandum
Author: Selected Technical Reports
Author: United States. Federal Aviation AdministrationPublisher:
ISBN:
Category :
Languages : en
Pages : 590
Book Description
The Calculation of Downwash Behind Supersonic Wings with an Application to Triangular Plan Forms
Author: Max A. HeasletPublisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 726
Book Description
A method is developed, consistent with the assumptions of small perturbation theory, which provides a means of determining for a known load distribution, the downwash behind a wing in supersonic flow. THe analysis is based upon the use of supersonic doublets which are distributed over the plan form and wake of the wing in a manner determined from the wing loading.