A Computational System For Aerodynamic Design And Analysis Of Supersonic Aircraft Part 3 Computer Program Description

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A computational system for aerodynamic design and analysis of supersonic aircraft

Author : Wilbur D. Middleton,J. L. Lundry,Robert Griffin Coleman
Publisher : Unknown
Page : 116 pages
File Size : 49,9 Mb
Release : 1976
Category : Aerodynamics, Supersonic
ISBN : UIUC:30112106859066

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A computational system for aerodynamic design and analysis of supersonic aircraft by Wilbur D. Middleton,J. L. Lundry,Robert Griffin Coleman Pdf

Aerodynamic Design and Analysis System for Supersonic Aircraft. Part 3: Computer Program Description

Author : Anonim
Publisher : Unknown
Page : 104 pages
File Size : 40,7 Mb
Release : 1975
Category : Electronic
ISBN : NASA:31769000525462

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Aerodynamic Design and Analysis System for Supersonic Aircraft. Part 3: Computer Program Description by Anonim Pdf

The computer program for the design and analysis of supersonic aircraft configurations is presented. The schematics of the program structure are provided. The individual overlays and subroutines are described. The system is useful in determining surface pressures and supersonic area rule concepts.

NASA Technical Memorandum

Author : Anonim
Publisher : Unknown
Page : 104 pages
File Size : 55,6 Mb
Release : 1980
Category : Aeronautics
ISBN : MINN:31951000845247A

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NASA Technical Memorandum by Anonim Pdf

NASA Technical Paper

Author : United States. National Aeronautics and Space Administration
Publisher : Unknown
Page : 824 pages
File Size : 42,6 Mb
Release : 1978
Category : Aeronautics
ISBN : UOM:39015004470921

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NASA Technical Paper by United States. National Aeronautics and Space Administration Pdf

NASA Technical Paper

Author : Anonim
Publisher : Unknown
Page : 124 pages
File Size : 42,8 Mb
Release : 1980
Category : Science
ISBN : STANFORD:36105024763893

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NASA Technical Paper by Anonim Pdf

Aerodynamic Characteristics at Mach Numbers of 1.5, 1.8, and 2.0 of a Blended Wing-body Configuration with and Without Integral Canards

Author : A. Warner Robins,Milton Lamb,David S. Miller
Publisher : Unknown
Page : 68 pages
File Size : 49,9 Mb
Release : 1979
Category : Hypersonic planes
ISBN : NASA:31769000429046

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Aerodynamic Characteristics at Mach Numbers of 1.5, 1.8, and 2.0 of a Blended Wing-body Configuration with and Without Integral Canards by A. Warner Robins,Milton Lamb,David S. Miller Pdf

NASA Reference Publication

Author : Anonim
Publisher : Unknown
Page : 754 pages
File Size : 55,6 Mb
Release : 1977
Category : Astronautics
ISBN : MINN:31951D00023633P

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NASA Reference Publication by Anonim Pdf

Computer Program Abstracts

Author : Anonim
Publisher : Unknown
Page : 30 pages
File Size : 51,9 Mb
Release : 1977
Category : Computer programs
ISBN : MINN:30000011049149

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Computer Program Abstracts by Anonim Pdf