Unsteady Transonic Aerodynamics of Pointed Bodies of Revolution in Supersonic Freestream

Unsteady Transonic Aerodynamics of Pointed Bodies of Revolution in Supersonic Freestream
Author :
Publisher :
Total Pages : 9
Release :
ISBN-10 : OCLC:228024793
ISBN-13 :
Rating : 4/5 ( Downloads)

Book Synopsis Unsteady Transonic Aerodynamics of Pointed Bodies of Revolution in Supersonic Freestream by : P. Garcia Fogeda

Download or read book Unsteady Transonic Aerodynamics of Pointed Bodies of Revolution in Supersonic Freestream written by P. Garcia Fogeda and published by . This book was released on 1992 with total page 9 pages. Available in PDF, EPUB and Kindle. Book excerpt: A method to determine the aerodynamic forces acting on oscillating pointed bodies of revolution in transonic-supersonic flight has been developed. The nonlinear equation for the mean-flow perturbation potential and the time linearized equation for the cross-flow perturbation potential are both of hyperbolic type, for the Mach number range of interest, and have been solved by the method of characteristics. The method is valid for arbitrary frequencies of oscillation and can be applied for rigid or flexible body motions. Results are presented for the stability force coefficients, unsteady pressure distributions and shock deformations for various body shapes and Mach numbers.


Unsteady Transonic Aerodynamics of Pointed Bodies of Revolution in Supersonic Freestream Related Books

Unsteady Transonic Aerodynamics of Pointed Bodies of Revolution in Supersonic Freestream
Language: en
Pages: 9
Authors: P. Garcia Fogeda
Categories:
Type: BOOK - Published: 1992 - Publisher:

DOWNLOAD EBOOK

A method to determine the aerodynamic forces acting on oscillating pointed bodies of revolution in transonic-supersonic flight has been developed. The nonlinear
Unsteady Aerodynamic Forces on a Slender Body of Revolution in Supersonic Flow
Language: en
Pages: 36
Authors: Reuben Bond
Categories: Aerodynamics, Supersonic
Type: BOOK - Published: 1961 - Publisher:

DOWNLOAD EBOOK

Linearized slender-body theory is applied to the computation of aerodynamic forces on an oscillating, or deforming, body in supersonic flow. The undeformed body
Unsteady Aerodynamics Forces on a Slender Body of Revolution in Supersonic Flow
Language: en
Pages: 32
Authors: Reuben Bond
Categories:
Type: BOOK - Published: 1961 - Publisher:

DOWNLOAD EBOOK

non- steady supersonic flow about pointed bodies of revolution
Language: en
Pages: 38
Authors: w. h. dorrance
Categories:
Type: BOOK - Published: 1950 - Publisher:

DOWNLOAD EBOOK

Boundary-layer Transition Study of Several Pointed Bodies of Revolution at Supersonic Speeds
Language: en
Pages: 76
Authors: William A. Cassels
Categories: Aerodynamics, Supersonic
Type: BOOK - Published: 1970 - Publisher:

DOWNLOAD EBOOK

Boundary-layer transition by the sublimation and impact-pressure techniques and force tests have been performed on three Haack-Adams bodies of revolution of fin