Author: Zdeněk Kopal
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 20
Book Description
A Few Remarks on the Limitations of Linearized Theory in Supersonic Flow
Author: Zdeněk Kopal
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 20
Book Description
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 20
Book Description
Linearized Theory of Supersonic Flow
Author: Sydney Goldstein
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 56
Book Description
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 56
Book Description
Linearized Theory of Steady High-Speed Flow
Author: G. N. Ward
Publisher: Cambridge University Press
ISBN: 1316601897
Category : Mathematics
Languages : en
Pages : 261
Book Description
Originally published in 1955, this book is devoted exclusively to the problems involved in solving the non-linear equations of motion for compressible fluids.
Publisher: Cambridge University Press
ISBN: 1316601897
Category : Mathematics
Languages : en
Pages : 261
Book Description
Originally published in 1955, this book is devoted exclusively to the problems involved in solving the non-linear equations of motion for compressible fluids.
linearized theory of steady high-speed flow
A Modification to Linearized Theory for Prediction of Pressure Loadings on Lifting Surfaces at High Supersonic Mach Numbers and Large Angles of Attack
Application of the Linearized Theory of Supersonic Flow to the Estimation of Control-Surface Characteristics
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 57
Book Description
Known conical-flow solutions of the linearized equation for the velocity potential in supersonic flow are applied to the calculation of the characteristics of control surfaces Complete solutions for the pressure distributions are obtained for control surfaces with hinge lines swept ahead of or behind the Mach line when the control-surface trailing edge is swept ahead of the Mach line. Useful approximate solutions of good accuracy are obtained when the trailing edge is swept behind the Mach line. Applications of the theory to the estimation of the hinge-moment and effectiveness characteristics of elevators and ailerons are presented.
Publisher:
ISBN:
Category :
Languages : en
Pages : 57
Book Description
Known conical-flow solutions of the linearized equation for the velocity potential in supersonic flow are applied to the calculation of the characteristics of control surfaces Complete solutions for the pressure distributions are obtained for control surfaces with hinge lines swept ahead of or behind the Mach line when the control-surface trailing edge is swept ahead of the Mach line. Useful approximate solutions of good accuracy are obtained when the trailing edge is swept behind the Mach line. Applications of the theory to the estimation of the hinge-moment and effectiveness characteristics of elevators and ailerons are presented.
Linearized Theory of Conical Supersonic Flow with Application to Triangular Wings
Author: North American Aviation, inc
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 122
Book Description
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 122
Book Description
Application of the Linearized Theory of Supersonic Flow to the Estimation of Control-surface Characteristics
Author: Charles W. Frick
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 56
Book Description
This report presents methods for computing control-surface characteristics at supersonic speeds for a variety of wing plan forms. The methods are developed for the velocity potential in supersonic flow and are subject to the usual limitations of the linear theory. The methods are applied to the calculation of the chordwise pressure distributions, lift coefficients, and hinge-moment coefficients for several types of control surfaces.
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 56
Book Description
This report presents methods for computing control-surface characteristics at supersonic speeds for a variety of wing plan forms. The methods are developed for the velocity potential in supersonic flow and are subject to the usual limitations of the linear theory. The methods are applied to the calculation of the chordwise pressure distributions, lift coefficients, and hinge-moment coefficients for several types of control surfaces.
A Modificiation to Linearized Theory for Prediction of Pressure Loadings on Lifting Surfaces at High Supersonic Mach Numbers and Large Angles of Attack
Author: Harry W. Carlson
Publisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 44
Book Description
Publisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 44
Book Description
Analysis of the Linearized Supersonic Flow about Pointed Bodies of Revolution by the Method of Characteristics
Author: Alan D. Sherer
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 52
Book Description
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 52
Book Description