Nonlinear Thermoelastic Effects on Hypersonic Stability and Control. Part I, Volume 2. Aerodynamics

Nonlinear Thermoelastic Effects on Hypersonic Stability and Control. Part I, Volume 2. Aerodynamics PDF Author: James R. Batt
Publisher:
ISBN:
Category :
Languages : en
Pages : 72

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Book Description
The curves presented in this volume of the final report are to be used to obtain aerodynamic influence coefficient matrices for slender two-dimensional airfoils in hypersonic inviscid flow. Influence coefficients are presented for ten airfoil shapes as a function of thickness ratio, Mach number and geometric angle of attack. (Author).

Nonlinear Thermoelastic Effects on Hypersonic Stability and Control. Part I, Volume 2. Aerodynamics

Nonlinear Thermoelastic Effects on Hypersonic Stability and Control. Part I, Volume 2. Aerodynamics PDF Author: James R. Batt
Publisher:
ISBN:
Category :
Languages : en
Pages : 72

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Book Description
The curves presented in this volume of the final report are to be used to obtain aerodynamic influence coefficient matrices for slender two-dimensional airfoils in hypersonic inviscid flow. Influence coefficients are presented for ten airfoil shapes as a function of thickness ratio, Mach number and geometric angle of attack. (Author).

Nonlinear Thermoelastic Effects on Hypersonic Stability and Control

Nonlinear Thermoelastic Effects on Hypersonic Stability and Control PDF Author: James R. Batt
Publisher:
ISBN:
Category :
Languages : en
Pages :

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Book Description


Nonlinear Thermoelastic Effects on Hypersonic Stability and Control

Nonlinear Thermoelastic Effects on Hypersonic Stability and Control PDF Author: James R. Batt
Publisher:
ISBN:
Category : Aerodynamics, Hypersonic
Languages : en
Pages : 86

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Thermoelastic Effects on Hypersonic Stability and Control: Hypersonic aerodynamics

Thermoelastic Effects on Hypersonic Stability and Control: Hypersonic aerodynamics PDF Author: James R. Batt
Publisher:
ISBN:
Category : Aerodynamics, Hypersonic
Languages : en
Pages : 392

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Thermoelastic Effects on Hypersonic Stability and Control: Hypersonic aeroelasticity

Thermoelastic Effects on Hypersonic Stability and Control: Hypersonic aeroelasticity PDF Author: James R. Batt
Publisher:
ISBN:
Category : Aerodynamics, Hypersonic
Languages : en
Pages : 190

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Technical Abstract Bulletin

Technical Abstract Bulletin PDF Author:
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 684

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Nonlinear Thermoelastic Effects on Hypersonic Stability and Control. Part Ii. Analytical and Experimental Static Aerothermoelasticity

Nonlinear Thermoelastic Effects on Hypersonic Stability and Control. Part Ii. Analytical and Experimental Static Aerothermoelasticity PDF Author: James R. Batt
Publisher:
ISBN:
Category :
Languages : en
Pages : 90

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An analytical method was developed for the analysis of static aerothermoelastic behavior in the presence of nonlinear aerodynamic loads and geometrically nonlinear structural behavior. The method was programmed for the IBM 7090 digital computer using FORTRAN coding techniques. A system for the experimental determination of static aerothermoelastic response of nonuniformly heated structures to loadings which are a nonlinear function of wing surface slopes was developed. Results of this experimental program are presented and compared with theoretical predictions. (Author).

Scientific and Technical Aerospace Reports

Scientific and Technical Aerospace Reports PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 702

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Government-wide Index to Federal Research & Development Reports

Government-wide Index to Federal Research & Development Reports PDF Author:
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 484

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Thermoelastic Effects on Hypersonic Stability and Control: v. 3. Elastic response analysis of fuselage and combined wing-fuselage structures

Thermoelastic Effects on Hypersonic Stability and Control: v. 3. Elastic response analysis of fuselage and combined wing-fuselage structures PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 88

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