Author: V. S. Nikolaev
Publisher:
ISBN:
Category : Aerodynamics, Hypersonic
Languages : en
Pages : 20
Book Description
Viscous Hypersonic Flow Past a Slender Cone
Author: V. S. Nikolaev
Publisher:
ISBN:
Category : Aerodynamics, Hypersonic
Languages : en
Pages : 20
Book Description
Publisher:
ISBN:
Category : Aerodynamics, Hypersonic
Languages : en
Pages : 20
Book Description
Viscous Hypersonic Flow Past a Slender Cone
Viscous Hypersonic Flow Past a Slender Cone
Author: V. S. Nikolaev
Publisher:
ISBN:
Category : Aerodynamics, Hypersonic
Languages : en
Pages : 0
Book Description
Publisher:
ISBN:
Category : Aerodynamics, Hypersonic
Languages : en
Pages : 0
Book Description
Viscous Hypersonic Flow Past Slender Cone [with List of References]
Author:
Publisher:
ISBN:
Category : Aerodynamics, Hypersonic
Languages : en
Pages : 7
Book Description
Publisher:
ISBN:
Category : Aerodynamics, Hypersonic
Languages : en
Pages : 7
Book Description
Viscous Hypersonic Flow Past a Slender Cone at Incidence
Author: Roberto Vaglio-Laurin
Publisher:
ISBN:
Category : Aerodynamics, Hypersonic
Languages : en
Pages : 10
Book Description
Publisher:
ISBN:
Category : Aerodynamics, Hypersonic
Languages : en
Pages : 10
Book Description
Viscous Hypersonic Flow Over Pointed Cones at Low Reynolds Numbers
Author: H. F. Waldron
Publisher:
ISBN:
Category : Aerodynamics, Hypersonic
Languages : en
Pages : 90
Book Description
Publisher:
ISBN:
Category : Aerodynamics, Hypersonic
Languages : en
Pages : 90
Book Description
Approximation of Hypersonic Flow Past a Slender Elliptic Cone
Viscous-shock-layer Analysis of Hypersonic Flows Over Long Slender Vehicles
Author: Kam-Pui Lee
Publisher:
ISBN:
Category : Fluid mechanics
Languages : en
Pages : 226
Book Description
Publisher:
ISBN:
Category : Fluid mechanics
Languages : en
Pages : 226
Book Description
Hypersonic Flow Over a Slender Cone
Author: John Kliewer Wall
Publisher:
ISBN:
Category : Boundary layer
Languages : en
Pages : 202
Book Description
Publisher:
ISBN:
Category : Boundary layer
Languages : en
Pages : 202
Book Description
Oscillating Slender Cone in Viscous Hypersonic Flow
Author: Kazimierz J. Orlik-Rueckemann
Publisher:
ISBN:
Category :
Languages : en
Pages : 3
Book Description
Unsteady pressure distributions and stability derivatives on a slender circular cone performing oscillation in pitch in viscous hypersonic flow can be determined using the method of dynamic viscous pressure interaction developed by the present author. The method takes into account the relative motion between the body surface and the boundary-layer displacement surface and can be applied to arbitrary bodies and flow conditions, provided the relevant inviscid unsteady pressure distributions and the dependence of the boundary-layer displacement on the steady flow variables are known. In the present paper, practical closed-form formulas are given for the unsteady pressure distribution and the static and dynamic pitching moment derivatives for a slender right circular cone performing low-frequency, small-amplitude oscillation in pitch around zero mean incidence and completely submerged in the weak-interaction region of laminar boundary layer. (Author).
Publisher:
ISBN:
Category :
Languages : en
Pages : 3
Book Description
Unsteady pressure distributions and stability derivatives on a slender circular cone performing oscillation in pitch in viscous hypersonic flow can be determined using the method of dynamic viscous pressure interaction developed by the present author. The method takes into account the relative motion between the body surface and the boundary-layer displacement surface and can be applied to arbitrary bodies and flow conditions, provided the relevant inviscid unsteady pressure distributions and the dependence of the boundary-layer displacement on the steady flow variables are known. In the present paper, practical closed-form formulas are given for the unsteady pressure distribution and the static and dynamic pitching moment derivatives for a slender right circular cone performing low-frequency, small-amplitude oscillation in pitch around zero mean incidence and completely submerged in the weak-interaction region of laminar boundary layer. (Author).