Author : Anonim
Publisher : Unknown
Page : 116 pages
File Size : 54,8 Mb
Release : 1976
Category : Electronic
ISBN : NASA:31769000498801
A Computational System For Aerodynamic Design And Analysis Of Supersonic Aircraft Part 3 Computer Program Description
A Computational System For Aerodynamic Design And Analysis Of Supersonic Aircraft Part 3 Computer Program Description Book in PDF, ePub and Kindle version is available to download in english. Read online anytime anywhere directly from your device. Click on the download button below to get a free pdf file of A Computational System For Aerodynamic Design And Analysis Of Supersonic Aircraft Part 3 Computer Program Description book. This book definitely worth reading, it is an incredibly well-written.
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
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
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
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
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
NASA Technical Paper by Anonim Pdf
A Modification to Linearized Theory for Prediction of Pressure Loadings on Lifting Surfaces at High Supersonic Mach Numbers and Large Angles of Attack
Author : Harry W. Carlson
Publisher : Unknown
Page : 44 pages
File Size : 51,8 Mb
Release : 1979
Category : Electronic
ISBN : NASA:31769000428840
A Modification to Linearized Theory for Prediction of Pressure Loadings on Lifting Surfaces at High Supersonic Mach Numbers and Large Angles of Attack by Harry W. Carlson Pdf
A Computational System for Aerodynamic Design and Analysis of Supersonic Aircraft. Part 1: General Description and Theoretical Development
Author : Anonim
Publisher : Unknown
Page : 88 pages
File Size : 48,7 Mb
Release : 1976
Category : Electronic
ISBN : NASA:31769000498785
A Computational System for Aerodynamic Design and Analysis of Supersonic Aircraft. Part 1: General Description and Theoretical Development by Anonim Pdf
Scientific and Technical Aerospace Reports
Author : Anonim
Publisher : Unknown
Page : 836 pages
File Size : 51,6 Mb
Release : 1994
Category : Aeronautics
ISBN : UIUC:30112067190055
Scientific and Technical Aerospace Reports by Anonim Pdf
Monthly Catalog of United States Government Publications
Author : Anonim
Publisher : Unknown
Page : 1194 pages
File Size : 48,7 Mb
Release : 1976
Category : Government publications
ISBN : UCR:31210024274613
Monthly Catalog of United States Government Publications 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
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
A Computational System for Aerodynamic Design and Analysis of Supersonic Aircraft. Part 2: User's Manual
Author : Anonim
Publisher : Unknown
Page : 276 pages
File Size : 54,9 Mb
Release : 1976
Category : Electronic
ISBN : NASA:31769000498793
A Computational System for Aerodynamic Design and Analysis of Supersonic Aircraft. Part 2: User's Manual by Anonim Pdf
NASA Reference Publication
Author : Anonim
Publisher : Unknown
Page : 754 pages
File Size : 55,6 Mb
Release : 1977
Category : Astronautics
ISBN : MINN:31951D00023633P
NASA Reference Publication by Anonim Pdf
A System for Aerodynamic Design and Analysis of Supersonic Aircraft: Computer program description
Author : Anonim
Publisher : Unknown
Page : 128 pages
File Size : 41,9 Mb
Release : 1980
Category : Aerodynamics, Supersonic
ISBN : UIUC:30112106860270
A System for Aerodynamic Design and Analysis of Supersonic Aircraft: Computer program description 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