Effects of Body Shape on the Aerodynamics of a Body of Revolution at Mach Numbers from 1.6 to 4.6 PDF Download

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Effects of Body Shape on the Aerodynamics of a Body of Revolution at Mach Numbers from 1.6 to 4.6

Effects of Body Shape on the Aerodynamics of a Body of Revolution at Mach Numbers from 1.6 to 4.6 PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 26

Book Description


Effects of Body Shape on the Aerodynamics of a Body of Revolution at Mach Numbers from 1.6 to 4.6

Effects of Body Shape on the Aerodynamics of a Body of Revolution at Mach Numbers from 1.6 to 4.6 PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 26

Book Description


Effect of Afterbody Geometry and Sting Diameter on the Aerodynamic Characteristics of Slender Bodies at Mach Number from 1.57 to 2.86

Effect of Afterbody Geometry and Sting Diameter on the Aerodynamic Characteristics of Slender Bodies at Mach Number from 1.57 to 2.86 PDF Author: Dennis E. Fuller
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 38

Book Description


Effect of Cross-section Shape on the Aerodynamics Characteristics of Bodies at Mach Numbers from 2.50 to 4.63

Effect of Cross-section Shape on the Aerodynamics Characteristics of Bodies at Mach Numbers from 2.50 to 4.63 PDF Author: Dennis E. Fuller
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 40

Book Description


The Flow Past a Straight- and a Swept-wing-body Combination and Their Equivalent Bodies of Revolution at Mach Numbers Near 1.0

The Flow Past a Straight- and a Swept-wing-body Combination and Their Equivalent Bodies of Revolution at Mach Numbers Near 1.0 PDF Author: W. F. Lindsey
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 24

Book Description
Abstract: The complete flow fields past a straight and a swept wing-body combination and their equivalent bodies of revolution at Mach numbers around 1.0 have been observed by means of motion-picture schlieren photography. The results of these observations indicate that the shock growth and positions on the wing-body combinations are closely reproduced in the flow past their respective equivalent bodies.

Aerodynamic Characteristics for Four Bodies of Revolution Showing Some Effects of Afterbody Shape and Fineness Ratio at Free-stream Mach Numbers from 1.50 to 1.99

Aerodynamic Characteristics for Four Bodies of Revolution Showing Some Effects of Afterbody Shape and Fineness Ratio at Free-stream Mach Numbers from 1.50 to 1.99 PDF Author: Robert J. Cohen
Publisher:
ISBN:
Category :
Languages : en
Pages : 31

Book Description


Calculated Pressure Distributions and Components of Total-drag Coefficients for 18 Constant-volume Slender Bodies of Revolution at Zero Incidence for Mach Numbers from 2.0 to 12.0, with Experimental Aerodynamic Characteristics for Three of the Bodies

Calculated Pressure Distributions and Components of Total-drag Coefficients for 18 Constant-volume Slender Bodies of Revolution at Zero Incidence for Mach Numbers from 2.0 to 12.0, with Experimental Aerodynamic Characteristics for Three of the Bodies PDF Author: Louis S. Stiver
Publisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 108

Book Description


Effects of Body Shape on the Aerodynamic Characteristics of an All-body Hypersonic Aircraft Configuration at Mach Numbers from 0.65 to 10.6

Effects of Body Shape on the Aerodynamic Characteristics of an All-body Hypersonic Aircraft Configuration at Mach Numbers from 0.65 to 10.6 PDF Author: Walter P. Nelms
Publisher:
ISBN:
Category : Drag (Aerodynamics)
Languages : en
Pages : 68

Book Description


Aerodynamic Characteristics, Including Effect of Body Shape, of a Mach 6 Aircraft Concept

Aerodynamic Characteristics, Including Effect of Body Shape, of a Mach 6 Aircraft Concept PDF Author: Gregory D. Riebe
Publisher:
ISBN:
Category : Aerodynamics, Hypersonic
Languages : en
Pages : 34

Book Description


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

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

Book Description


Index to NASA Technical Publications

Index to NASA Technical Publications PDF Author: United States. National Aeronautics and Space Administration
Publisher:
ISBN:
Category :
Languages : en
Pages : 208

Book Description