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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
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 562

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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
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 562

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Book Description

Technical Note

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

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Measurements of Aerodynamic Heating Obtained During Demonstration Flight Tests of the Douglas D-558-II Airplane

Measurements of Aerodynamic Heating Obtained During Demonstration Flight Tests of the Douglas D-558-II Airplane PDF Author: Ira P. Jones
Publisher:
ISBN:
Category : Aerodynamic heating
Languages : en
Pages : 26

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Annual Report of the National Advisory Committee for Aeronautics

Annual Report of the National Advisory Committee for Aeronautics PDF Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 988

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

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 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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Index of NACA Technical Publications

Index of NACA Technical Publications PDF Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1370

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Method for Determining the Frequency-response Characteristics of an Element of System from the System Transient Output Response to a Known Input Function

Method for Determining the Frequency-response Characteristics of an Element of System from the System Transient Output Response to a Known Input Function PDF Author: Charles W. Matthews
Publisher:
ISBN:
Category : Aerofoils
Languages : en
Pages : 196

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WADC Technical Report

WADC Technical Report PDF Author: United States. Wright Air Development Division
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1286

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Use of a Characteristic Surfaces for Unisymmetrical Supersonic Flow Problems

Use of a Characteristic Surfaces for Unisymmetrical Supersonic Flow Problems PDF Author: W. E. Moeckel
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 674

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Book Description
Application of the method of characteristics to the linearized three-dimensional equation results in a relatively simple system of difference equations that can be used to compute the supersonic flow past boundaries for which no other linearized solutions are available.