Author: E. A. Brong
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 104
Book Description
The Unsteady Flow Field about a Right Circular Cone in Unsteady Flight
Author: E. A. Brong
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 104
Book Description
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 104
Book Description
NASA Technical Report
Author: United States. National Aeronautics and Space Administration
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 936
Book Description
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 936
Book Description
Government-wide Index to Federal Research & Development Reports
Author:
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1470
Book Description
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1470
Book Description
Scientific and Technical Aerospace Reports
Unsteady Newton-Busemann Flow Theory. Part 2: Bodies of Revolution
Technical Abstract Bulletin
Author: Defense Documentation Center (U.S.)
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 784
Book Description
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 784
Book Description
Journal of the Royal Aeronautical Society
The Aeronautical Journal
Hypersonic Dynamic Stability
Author: L. A. Marshall
Publisher:
ISBN:
Category : Aerodynamics, Hypersonic
Languages : en
Pages : 98
Book Description
The report presents a summary of the important results obtained on a combined analytical and experimental program for investigation of the hypersonic dynamic stability of re-entry vehicles. An unsteady flow field solution is described which predicts the static and dynamic stability characteristics for vehicles which are executing small amplitude oscillations about zero angle of attack. Solutions were obtained for sharp and blunted, axisymmetric and two-dimensional shapes in real gas equilibrium flow. The experimental program was conducted in AEDC tunnel 'C' at Mach 10 and in the Ling-Temco-Vought Hot Shot tunnel at Mach 14 and 20 to obtain dynamic stability characteristics of a 10 degree cone. Data are presented to show the effect of bluntness ratio, reduced frequency, center of gravity location, Reynolds number and Mach number. Comparisons are made with various theoretical results and limited correlations are shown which establish significant trends.
Publisher:
ISBN:
Category : Aerodynamics, Hypersonic
Languages : en
Pages : 98
Book Description
The report presents a summary of the important results obtained on a combined analytical and experimental program for investigation of the hypersonic dynamic stability of re-entry vehicles. An unsteady flow field solution is described which predicts the static and dynamic stability characteristics for vehicles which are executing small amplitude oscillations about zero angle of attack. Solutions were obtained for sharp and blunted, axisymmetric and two-dimensional shapes in real gas equilibrium flow. The experimental program was conducted in AEDC tunnel 'C' at Mach 10 and in the Ling-Temco-Vought Hot Shot tunnel at Mach 14 and 20 to obtain dynamic stability characteristics of a 10 degree cone. Data are presented to show the effect of bluntness ratio, reduced frequency, center of gravity location, Reynolds number and Mach number. Comparisons are made with various theoretical results and limited correlations are shown which establish significant trends.
Dynamic Viscous Interaction in Hypersonic Flow
Author: Kazimierz J. Orlick-Rückemann
Publisher:
ISBN:
Category : Aerodynamics, Hypersonic
Languages : en
Pages : 96
Book Description
Publisher:
ISBN:
Category : Aerodynamics, Hypersonic
Languages : en
Pages : 96
Book Description