An Improved Method for the Aerodynamic Analysis of Wing-body-tail Configurations in Subsonic and Supersonic Flow. Part 2: Computer Program Description

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Total Pages : 326 pages
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Book Synopsis An Improved Method for the Aerodynamic Analysis of Wing-body-tail Configurations in Subsonic and Supersonic Flow. Part 2: Computer Program Description by : F. A. Woodward

Download or read book An Improved Method for the Aerodynamic Analysis of Wing-body-tail Configurations in Subsonic and Supersonic Flow. Part 2: Computer Program Description written by F. A. Woodward and published by . This book was released on 1973 with total page 326 pages. Available in PDF, EPUB and Kindle. Book excerpt:

An Improved Method for the Aerodynamic Analysis of Wing-body-tail Configurations in Subsonic and Supersonic Flow. Part 1: Theory and Application

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Total Pages : 140 pages
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Book Synopsis An Improved Method for the Aerodynamic Analysis of Wing-body-tail Configurations in Subsonic and Supersonic Flow. Part 1: Theory and Application by :

Download or read book An Improved Method for the Aerodynamic Analysis of Wing-body-tail Configurations in Subsonic and Supersonic Flow. Part 1: Theory and Application written by and published by . This book was released on 1973 with total page 140 pages. Available in PDF, EPUB and Kindle. Book excerpt:

An Improved Method for the Aerodynamic Analysis of Wing-body-tail Configurations in Subsonic and Supersonic Flow

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ISBN 13 :
Total Pages : 140 pages
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Book Synopsis An Improved Method for the Aerodynamic Analysis of Wing-body-tail Configurations in Subsonic and Supersonic Flow by : F. A. Woodward

Download or read book An Improved Method for the Aerodynamic Analysis of Wing-body-tail Configurations in Subsonic and Supersonic Flow written by F. A. Woodward and published by . This book was released on 1973 with total page 140 pages. Available in PDF, EPUB and Kindle. Book excerpt: A new method has been developed for calculating the pressure distribution and aerodynamic characteristics of wing-body-tail combinations in subsonic and supersonic potential flow. A computer program has been developed to perform the numerical calculations. The configuration surface is subdivided into a large number of panels, each of which contains an aerodynamic singularity distribution. A constant source distribution is used on the body panels, and a vortex distribution having a linear variation in the streamwise direction is used on the wing and tail panels. The normal components of velocity induced at specified control points by each singularity distribution are calculated and make up the coefficients of a system of linear equations relating the strengths of the singularities to the magnitude of the normal velocities.

NASA Technical Paper

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Total Pages : 62 pages
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NASA Technical Memorandum

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Total Pages : 220 pages
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Book Synopsis NASA Technical Memorandum by :

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NASA Technical Note

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Total Pages : 772 pages
Book Rating : 4.3/5 (91 download)

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Download or read book NASA Technical Note written by and published by . This book was released on 1976 with total page 772 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Monthly Catalog of United States Government Publications, Cumulative Index

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Total Pages : 1408 pages
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Book Synopsis Monthly Catalog of United States Government Publications, Cumulative Index by : United States. Superintendent of Documents

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A Modification to Linearized Theory for Prediction of Pressure Loadings on Lifting Surfaces at High Supersonic Mach Numbers and Large Angles of Attack

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Total Pages : 44 pages
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Book Synopsis 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

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COSMIC

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ISBN 13 :
Total Pages : 168 pages
Book Rating : 4.3/5 ( download)

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Book Synopsis COSMIC by : United States. National Aeronautics and Space Administration

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Scientific and Technical Aerospace Reports

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ISBN 13 :
Total Pages : 704 pages
Book Rating : 4.:/5 (31 download)

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NASA Technical Paper

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ISBN 13 :
Total Pages : 380 pages
Book Rating : 4.3/5 (91 download)

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Book Synopsis NASA Technical Paper by : United States. National Aeronautics and Space Administration

Download or read book NASA Technical Paper written by United States. National Aeronautics and Space Administration and published by . This book was released on 1990 with total page 380 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Improved Method for Prediction of Attainable Wing Leading-Edge Thrust

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Total Pages : 70 pages
Book Rating : 4.:/5 (317 download)

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Book Synopsis Improved Method for Prediction of Attainable Wing Leading-Edge Thrust by : Harry W. Carlson

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Computer Program Abstracts

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Total Pages : 28 pages
Book Rating : 4.:/5 (3 download)

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Transonic Aerodynamic Characteristics of a Supersonic Cruise Aircraft Research Model with the Engines Suspended Above the Wing

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ISBN 13 :
Total Pages : 204 pages
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Book Synopsis Transonic Aerodynamic Characteristics of a Supersonic Cruise Aircraft Research Model with the Engines Suspended Above the Wing by : Charles E. Mercer

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Cumulative Index to NASA Tech Briefs

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ISBN 13 :
Total Pages : 788 pages
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Book Synopsis Cumulative Index to NASA Tech Briefs by : United States. National Aeronautics and Space Administration

Download or read book Cumulative Index to NASA Tech Briefs written by United States. National Aeronautics and Space Administration and published by . This book was released on 1970 with total page 788 pages. Available in PDF, EPUB and Kindle. Book excerpt:

NASA Tech Brief

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ISBN 13 :
Total Pages : 792 pages
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Download or read book NASA Tech Brief written by and published by . This book was released on 1970 with total page 792 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Bibliography on Aerodynamics of Airframe/engine Integration of High-speed Turbine-powered Aircraft

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ISBN 13 :
Total Pages : 100 pages
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Book Synopsis Bibliography on Aerodynamics of Airframe/engine Integration of High-speed Turbine-powered Aircraft by : Mark R. Nichols

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