NASA Technical Note

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ISBN 13 :
Total Pages : 558 pages
Book Rating : 4.:/5 (319 download)

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Book Synopsis NASA Technical Note by :

Download or read book NASA Technical Note written by and published by . This book was released on 1969 with total page 558 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Investigation of Laminar and Turbulent Boundary Layers Interacting with Externally Generated Shock Waves

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ISBN 13 :
Total Pages : 140 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis Investigation of Laminar and Turbulent Boundary Layers Interacting with Externally Generated Shock Waves by : Earl C. Watson

Download or read book Investigation of Laminar and Turbulent Boundary Layers Interacting with Externally Generated Shock Waves written by Earl C. Watson and published by . This book was released on 1969 with total page 140 pages. Available in PDF, EPUB and Kindle. Book excerpt: Laminar and turbulent boundary layer interactions with externally generated shock waves.

Hypersonic Aerodynamic Characteristics of Two Delta-wing X-15 Airplane Configurations

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ISBN 13 :
Total Pages : 108 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis Hypersonic Aerodynamic Characteristics of Two Delta-wing X-15 Airplane Configurations by : Theodore J. Goldberg

Download or read book Hypersonic Aerodynamic Characteristics of Two Delta-wing X-15 Airplane Configurations written by Theodore J. Goldberg and published by . This book was released on 1969 with total page 108 pages. Available in PDF, EPUB and Kindle. Book excerpt: Hypersonic aerodynamic characteristics of delta wing x- 15 airplane configurations.

Pressure Distributions on Two-dimensional Sharp-leading-edge Flat Plates with Sweep Angles of 0 Degrees, 30 Degrees, and 45 Degrees at a Mach Number of 6 and Angles of Attack from 0 Degrees to 90 Degrees

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ISBN 13 :
Total Pages : 28 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis Pressure Distributions on Two-dimensional Sharp-leading-edge Flat Plates with Sweep Angles of 0 Degrees, 30 Degrees, and 45 Degrees at a Mach Number of 6 and Angles of Attack from 0 Degrees to 90 Degrees by : James G. Hondros

Download or read book Pressure Distributions on Two-dimensional Sharp-leading-edge Flat Plates with Sweep Angles of 0 Degrees, 30 Degrees, and 45 Degrees at a Mach Number of 6 and Angles of Attack from 0 Degrees to 90 Degrees written by James G. Hondros and published by . This book was released on 1962 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt:

A Real-gas Study of Low-density Wedge-induced Laminar Separation on a Highly Cooled Blunt Flat Plate at M [infinity]

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ISBN 13 :
Total Pages : 42 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis A Real-gas Study of Low-density Wedge-induced Laminar Separation on a Highly Cooled Blunt Flat Plate at M [infinity] by : John Benjamin Anders

Download or read book A Real-gas Study of Low-density Wedge-induced Laminar Separation on a Highly Cooled Blunt Flat Plate at M [infinity] written by John Benjamin Anders and published by . This book was released on 1968 with total page 42 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Base Pressure Coefficients Obtained from the X-15 Airplane for Mach Numbers Up to 6

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ISBN 13 :
Total Pages : 56 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis Base Pressure Coefficients Obtained from the X-15 Airplane for Mach Numbers Up to 6 by : Edwin J. Saltzman

Download or read book Base Pressure Coefficients Obtained from the X-15 Airplane for Mach Numbers Up to 6 written by Edwin J. Saltzman and published by . This book was released on 1964 with total page 56 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Journal of the Royal Aeronautical Society

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ISBN 13 :
Total Pages : 1304 pages
Book Rating : 4.:/5 (318 download)

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Book Synopsis Journal of the Royal Aeronautical Society by :

Download or read book Journal of the Royal Aeronautical Society written by and published by . This book was released on 1966 with total page 1304 pages. Available in PDF, EPUB and Kindle. Book excerpt:

The Interaction of a Shock Wave with a Laminar Boundary Layer

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ISBN 13 :
Total Pages : 206 pages
Book Rating : 4.F/5 ( download)

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Book Synopsis The Interaction of a Shock Wave with a Laminar Boundary Layer by : Theodore A. Reyhner

Download or read book The Interaction of a Shock Wave with a Laminar Boundary Layer written by Theodore A. Reyhner and published by . This book was released on 1966 with total page 206 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Separated Flows

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ISBN 13 :
Total Pages : 270 pages
Book Rating : 4.:/5 (318 download)

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Book Synopsis Separated Flows by :

Download or read book Separated Flows written by and published by . This book was released on 1966 with total page 270 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Scientific and Technical Aerospace Reports

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ISBN 13 :
Total Pages : 1492 pages
Book Rating : 4.U/5 (183 download)

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Book Synopsis Scientific and Technical Aerospace Reports by :

Download or read book Scientific and Technical Aerospace Reports written by and published by . This book was released on 1966 with total page 1492 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Pressure Distribution on a Flat-bottom Canted Nose Half-cone Reentry Configuration at a Mach Number of 6.0

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ISBN 13 :
Total Pages : 28 pages
Book Rating : 4.:/5 (317 download)

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Book Synopsis Pressure Distribution on a Flat-bottom Canted Nose Half-cone Reentry Configuration at a Mach Number of 6.0 by :

Download or read book Pressure Distribution on a Flat-bottom Canted Nose Half-cone Reentry Configuration at a Mach Number of 6.0 written by and published by . This book was released on 1962 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Control of Flow Separation

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Publisher : Hemisphere Pub
ISBN 13 :
Total Pages : 556 pages
Book Rating : 4.F/5 ( download)

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Book Synopsis Control of Flow Separation by : Paul K. Chang

Download or read book Control of Flow Separation written by Paul K. Chang and published by Hemisphere Pub. This book was released on 1976 with total page 556 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Separated Flows

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ISBN 13 :
Total Pages : 498 pages
Book Rating : 4.0/5 ( download)

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Book Synopsis Separated Flows by : Jean J. Ginoux

Download or read book Separated Flows written by Jean J. Ginoux and published by . This book was released on 1966 with total page 498 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Proceedings of the ... International Heat Transfer Conference

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ISBN 13 :
Total Pages : 398 pages
Book Rating : 4.3/5 (91 download)

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Book Synopsis Proceedings of the ... International Heat Transfer Conference by :

Download or read book Proceedings of the ... International Heat Transfer Conference written by and published by . This book was released on 1967 with total page 398 pages. Available in PDF, EPUB and Kindle. Book excerpt:

AGARD Conference Proceedings

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ISBN 13 :
Total Pages : 492 pages
Book Rating : 4.X/5 (3 download)

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Book Synopsis AGARD Conference Proceedings by : North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development

Download or read book AGARD Conference Proceedings written by North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development and published by . This book was released on 1966 with total page 492 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Pressure Distribution on a Blunt-leading-edge Modified-delta-planform Reentry Configuration at a Mach Number of 6.0

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ISBN 13 :
Total Pages : 32 pages
Book Rating : 4.:/5 (317 download)

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Book Synopsis Pressure Distribution on a Blunt-leading-edge Modified-delta-planform Reentry Configuration at a Mach Number of 6.0 by :

Download or read book Pressure Distribution on a Blunt-leading-edge Modified-delta-planform Reentry Configuration at a Mach Number of 6.0 written by and published by . This book was released on 1963 with total page 32 pages. Available in PDF, EPUB and Kindle. Book excerpt:

USAF Stability and Control Datcom

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ISBN 13 :
Total Pages : 684 pages
Book Rating : 4.3/5 (91 download)

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Book Synopsis USAF Stability and Control Datcom by : Douglas Aircraft Company

Download or read book USAF Stability and Control Datcom written by Douglas Aircraft Company and published by . This book was released on 1975 with total page 684 pages. Available in PDF, EPUB and Kindle. Book excerpt: