Comparison of the Experimental and Theoretical Distributions of Lift on a Slender Inclined Body of Revolution at M

Comparison of the Experimental and Theoretical Distributions of Lift on a Slender Inclined Body of Revolution at M PDF Author: Edward W. Perkins
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ISBN:
Category : Aerodynamics
Languages : en
Pages : 46

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Abstract: An investigation of the pressure distribution for a body of revolution, consisting of a 33-1/3-caliber (5.75 fineness ratio) tangent ogival nose and a cylindrical afterbody, has been made for an angle-of-attack range of 0° to 35.5° at a Mach number of 1.98 and a Reynolds number of approximately 0.5 x 106m based on body diameter. Comparisons of the theoretical and experimental pressure distributions are made to show the nature of the effects of both viscosity and cross-flow compressibility. The experimental load distributions are compared with those predicted by the method suggested in NACA RM A9I26 which includes an approximate method for taking into account the effects of viscosity on the lift distribution.

Comparison of the Experimental and Theoretical Distributions of Lift on a Slender Inclined Body of Revolution at M

Comparison of the Experimental and Theoretical Distributions of Lift on a Slender Inclined Body of Revolution at M PDF Author: Edward W. Perkins
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 46

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Book Description
Abstract: An investigation of the pressure distribution for a body of revolution, consisting of a 33-1/3-caliber (5.75 fineness ratio) tangent ogival nose and a cylindrical afterbody, has been made for an angle-of-attack range of 0° to 35.5° at a Mach number of 1.98 and a Reynolds number of approximately 0.5 x 106m based on body diameter. Comparisons of the theoretical and experimental pressure distributions are made to show the nature of the effects of both viscosity and cross-flow compressibility. The experimental load distributions are compared with those predicted by the method suggested in NACA RM A9I26 which includes an approximate method for taking into account the effects of viscosity on the lift distribution.

Comparison of the Experimental and Theoretical Distributions of Lift on a Slender Inclined Body of Revolution at M

Comparison of the Experimental and Theoretical Distributions of Lift on a Slender Inclined Body of Revolution at M PDF Author: Edward W. Perkins
Publisher:
ISBN:
Category :
Languages : en
Pages : 39

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Technical Note - National Advisory Committee for Aeronautics

Technical Note - National Advisory Committee for Aeronautics PDF Author: United States. National Advisory Committee for Aeronautics
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Category : Aeronautics
Languages : en
Pages : 878

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Research Abstracts and Reclassification Notice

Research Abstracts and Reclassification Notice PDF Author: United States. National Advisory Committee for Aeronautics
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Category : Aeronautics
Languages : en
Pages : 508

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Monthly Catalog of United States Government Publications

Monthly Catalog of United States Government Publications PDF Author: United States. Superintendent of Documents
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Category : Government publications
Languages : en
Pages : 1640

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Report

Report PDF Author:
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ISBN:
Category : Aeronautics
Languages : en
Pages : 900

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Annual Report

Annual Report PDF Author: United States. National Advisory Committee for Aeronautics
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Category : Aeronautics
Languages : en
Pages : 534

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Annual Report - National Advisory Committee for Aeronautics

Annual Report - National Advisory Committee for Aeronautics PDF Author: United States. National Advisory Committee for Aeronautics
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Category : Aeronautics
Languages : en
Pages :

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Includes the Committee's Technical reports no. 1-1058, reprinted in v. 1-37.

Index of NACA Technical Publications

Index of NACA Technical Publications PDF Author: United States. National Advisory Committee for Aeronautics
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Category : Aeronautics
Languages : en
Pages : 580

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A Selected Listing of NASA Scientific and Technical Reports for ...

A Selected Listing of NASA Scientific and Technical Reports for ... PDF Author:
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Category : Aeronautics
Languages : en
Pages : 818

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