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
Author: Louis S. Stivers
Publisher:
Total Pages: 96
Release: 1971
Genre: Aerodynamic load
ISBN:
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Pressure distributions and drag coefficients of 18 constant length and volume slender bodies of revolution at zero incidence for Mach numbers 2.0 to 12.0 - graphs.


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
Language: en
Pages: 96

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

Authors: Louis S. Stivers
Categories: Aerodynamic load
Type: BOOK - Published: 1971 - Publisher:

GET EBOOK

Pressure distributions and drag coefficients of 18 constant length and volume slender bodies of revolution at zero incidence for Mach numbers 2.0 to 12.0 - grap
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
Language: en
Pages: 108

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

Authors: Louis S. Stiver
Categories: Aerodynamic load
Type: BOOK - Published: 1971 - Publisher:

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Government Reports Index
Language: en
Pages: 1088

Government Reports Index

Authors:
Categories: Government publications
Type: BOOK - Published: 1972 - Publisher:

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Handbook of Supersonic Aerodynamics
Language: en
Pages: 516

Handbook of Supersonic Aerodynamics

Authors: Johns Hopkins University. Applied Physics Laboratory, Silver Spring, Md
Categories: Aerodynamics, Supersonic
Type: BOOK - Published: 1961 - Publisher:

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Theoretical Pressure Distributions on Wings of Finite Span at Zero Incidence for Mach Numbers Near 1
Language: en
Pages: 58

Theoretical Pressure Distributions on Wings of Finite Span at Zero Incidence for Mach Numbers Near 1

Authors: Alberta Y. Alksne
Categories: Aerodynamics, Transonic
Type: BOOK - Published: 1961 - Publisher:

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A method employed heretofore by the authors to obtain approximate solutions of the transonic flow equation for plane and axisymmetric flow is extended to give r