Author: Varun SinghPublisher:
ISBN:
Category :
Languages : en
Pages : 162
Book Description
Numerical Simulation of Two-dimensional and Three-dimensional Secondary Flow in a Weakly Ionized Supersonic Flow with Applied Electromagnetic Field
Author: Varun SinghNumerical Simulation of Steady Supersonic Flow
Author: Numerical Simulation of Three-dimensional Supersonic Inlet Flow Fields
Author: T. KawamuraNumerical Simulation of Supersonic Flow Over a Three-dimensional Cavity
Author: D.P. RizzetaNumerical Simulation of Three-dimensional Supersonic Flows Using Euler and Boundary Layer Solvers
Author: F. Gaible36th AIAA Plasmadynamics and Lasers Conference: 05-5037 - 05-5390
Author: Scientific and Technical Aerospace Reports
Author: Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1126
Book Description
Lists citations with abstracts for aerospace related reports obtained from world wide sources and announces documents that have recently been entered into the NASA Scientific and Technical Information Database.
On Two-dimensional Supersonic Flows
Author: Stefan BergmanPublisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 56
Book Description
In previous reports by the author, the method of operators has been applied to investigation of two-dimensional flow patterns of an ideal compressible fluid, mostly in the subsonic case. Using a similar approach in the present paper, the author defines two different operators which generate supersonic two-dimensional flow patterns from differentiable functions of one real variable. (An operator is any rul by means of which one function is converted into another.) Since operators of the type considered preserve many properties of the functions to which they are applied and since the theory of functions of one real variable is more extensively developed than that of solutions of the compressibility equations, the results can be used as a basis for investigation of supersonic flow patterns.
Use of a Characteristic Surfaces for Unsymmetrical Supersonic Flow Problems
Author: Wolfgang E. MoeckelPublisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 56
Book Description
Application of the method of characteristics to the linearized three-dimensional equation results in a relatively simple system of difference equations that can be used to compute the supersonic flow past boundaries for which no other linearized solutions are available.
Author: F. Walkden