Afterbody Drag Investigation of a Twin-nozzle Fighter-type Model at Mach Numbers from 0.6 to 1.5 PDF Download

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Afterbody Drag Investigation of a Twin-nozzle Fighter-type Model at Mach Numbers from 0.6 to 1.5

Afterbody Drag Investigation of a Twin-nozzle Fighter-type Model at Mach Numbers from 0.6 to 1.5 PDF Author: Earl A. Price (Jr.)
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 122

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Afterbody Drag Investigation of a Twin-nozzle Fighter-type Model at Mach Numbers from 0.6 to 1.5

Afterbody Drag Investigation of a Twin-nozzle Fighter-type Model at Mach Numbers from 0.6 to 1.5 PDF Author: Earl A. Price (Jr.)
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 122

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NASA Technical Paper

NASA Technical Paper PDF Author:
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 218

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NASA Technical Memorandum

NASA Technical Memorandum PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 562

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A Parametric Investigation of the Annular Jet Concept for Obtaining Afterbody Drag Data at Transonic Mach Numbers

A Parametric Investigation of the Annular Jet Concept for Obtaining Afterbody Drag Data at Transonic Mach Numbers PDF Author: Earl A. Price (Jr.)
Publisher:
ISBN:
Category : Drag (Aerodynamics)
Languages : en
Pages : 182

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Afterbody/nozzle Pressure Distributions of a Twin-tail Twin-engine Fighter with Axisymmetric Nozzles at Mach Numbers from 0.6 to 1.2

Afterbody/nozzle Pressure Distributions of a Twin-tail Twin-engine Fighter with Axisymmetric Nozzles at Mach Numbers from 0.6 to 1.2 PDF Author: David J. Wing
Publisher:
ISBN:
Category :
Languages : en
Pages : 220

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Category : Government publications
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Pages : 1248

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Monthly Catalogue, United States Public Documents

Monthly Catalogue, United States Public Documents PDF Author:
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ISBN:
Category : Government publications
Languages : en
Pages : 1252

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Parametric Study of Afterbody/nozzle Drag on Twin Two-dimensional Convergent-divergent Nozzles at Mach Numbers from 0.60 to 1.20

Parametric Study of Afterbody/nozzle Drag on Twin Two-dimensional Convergent-divergent Nozzles at Mach Numbers from 0.60 to 1.20 PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 272

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Technical Abstract Bulletin

Technical Abstract Bulletin PDF Author:
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ISBN:
Category : Science
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Pages : 484

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