A Method for Determining the Aerodynamic Characteristics of Two- and Three-dimensional Shapes at Hypersonic Speeds

A Method for Determining the Aerodynamic Characteristics of Two- and Three-dimensional Shapes at Hypersonic Speeds PDF Author: H. Reese Ivey
Publisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 28

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Book Description
A method is developed for calculating the pressures on aerodynamic shapes at very high supersonic speeds in dense air with the ratio of specific heats equal to 1. The method is applicable to any body of revolution at zero angle of attack and to any two-dimensional profile. The results of the present paper are compared with previous work of Von Karman and Epstein on this problem and the difference explained.

A Method for Determining the Aerodynamic Characteristics of Two- and Three-dimensional Shapes at Hypersonic Speeds

A Method for Determining the Aerodynamic Characteristics of Two- and Three-dimensional Shapes at Hypersonic Speeds PDF Author: H. Reese Ivey
Publisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 28

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Book Description
A method is developed for calculating the pressures on aerodynamic shapes at very high supersonic speeds in dense air with the ratio of specific heats equal to 1. The method is applicable to any body of revolution at zero angle of attack and to any two-dimensional profile. The results of the present paper are compared with previous work of Von Karman and Epstein on this problem and the difference explained.

A Method for Determining the Aerodynamic Characteristics of Two- and Three-dimensional Shapes at Hypersonic Speeds

A Method for Determining the Aerodynamic Characteristics of Two- and Three-dimensional Shapes at Hypersonic Speeds PDF Author: F. Reese Ivey
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 21

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Some aerodynamic characteristics of several shapes are calculated, and it is shown that the lift and drag coefficients are dependent upon the thickness ratio, thickness distribution, and angle of attack.

Technical Note

Technical Note PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 388

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NASA Scientific and Technical Reports

NASA Scientific and Technical Reports PDF Author: United States. National Aeronautics and Space Administration Scientific and Technical Information Division
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ISBN:
Category : Aeronautics
Languages : en
Pages : 2300

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Report

Report PDF Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 40

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Experimental Pressure Distributions Over Blunt Two- and Three-dimensional Bodies Having Similar Cross Sections at a Mach Number of 4.95

Experimental Pressure Distributions Over Blunt Two- and Three-dimensional Bodies Having Similar Cross Sections at a Mach Number of 4.95 PDF Author: Jerome D. Julius
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ISBN:
Category :
Languages : en
Pages : 22

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Theoretical and Analog Studies of the Effects of Nonlinear Stability Derivatives on the Longitudinal Motions of an Aircraft in Response to Step Control Deflections and to the Influence of Proportional Automatic Control

Theoretical and Analog Studies of the Effects of Nonlinear Stability Derivatives on the Longitudinal Motions of an Aircraft in Response to Step Control Deflections and to the Influence of Proportional Automatic Control PDF Author: Benjamin Milwitzky
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ISBN:
Category : Aeronautics
Languages : en
Pages : 348

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The Effect of Blade-section Thickness Ratios on the Aerodynamic Characteristics of Related Full-scale Propellers at Mach Numbers Up to 0.65

The Effect of Blade-section Thickness Ratios on the Aerodynamic Characteristics of Related Full-scale Propellers at Mach Numbers Up to 0.65 PDF Author: A. J. Eggers
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 286

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Report

Report PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 962

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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:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 664

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Book Description