Author: Douglas Dilley
Publisher:
ISBN:
Category :
Languages : en
Pages : 428
Book Description
A Numerical Study of Several Supersonic Flows
Author: Douglas Dilley
Publisher:
ISBN:
Category :
Languages : en
Pages : 428
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 428
Book Description
A Numerical Study of Supersonic Flow Over a Compression Corner with Different Incoming Boundary Layer Profiles
Author: S. C. Holmes
Publisher:
ISBN:
Category :
Languages : en
Pages :
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages :
Book Description
Numerical Study of Supersonic Flows Using Different Techniques
Author: Gary W. Huband (CAPT, USAF.)
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 150
Book Description
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 150
Book Description
Numerical Study of Supersonic Flows Using Different Techniques
Author: Gary W. Huband
Publisher:
ISBN:
Category :
Languages : en
Pages : 85
Book Description
The purpose of this work was to obtain the solution to three supersonic flow problems using three different numerical techniques. First, a shock/boundary layer problem is solved using MacCormack's explicit technique. Then, using the same technique a shrouded rocket nozzle problem is solved. These two problems showed that the explicit scheme required many minutes of computer time to solve. In order to explore more efficient codes to solve the shroud problem, space marching algorithms were studied. A space marching algorithm using flux-splitting in the streamwise direction was applied to an approximate form of the Navier-Stokes equation. Flux-splitting combined with a global interation approach should allow the shroud problem to be solved with a space marching algorithm. The flux-splitting code was applied to two supersonic flow problems and very good results were obtained. (Author) (Theses).
Publisher:
ISBN:
Category :
Languages : en
Pages : 85
Book Description
The purpose of this work was to obtain the solution to three supersonic flow problems using three different numerical techniques. First, a shock/boundary layer problem is solved using MacCormack's explicit technique. Then, using the same technique a shrouded rocket nozzle problem is solved. These two problems showed that the explicit scheme required many minutes of computer time to solve. In order to explore more efficient codes to solve the shroud problem, space marching algorithms were studied. A space marching algorithm using flux-splitting in the streamwise direction was applied to an approximate form of the Navier-Stokes equation. Flux-splitting combined with a global interation approach should allow the shroud problem to be solved with a space marching algorithm. The flux-splitting code was applied to two supersonic flow problems and very good results were obtained. (Author) (Theses).
A Numerical Study on Mixing of Supersonic Flow Field with Parallel Injection Through Ramp Nozzle
Author: Yoshiyuki Yamane
Publisher:
ISBN:
Category :
Languages : en
Pages :
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages :
Book Description
Numerical Study of Control of Dynamic Properties of a Supersonic Inlet Using Bypass Bleed
Author: Clarence W. Matthews
Publisher:
ISBN:
Category : Automatic control
Languages : en
Pages : 44
Book Description
Publisher:
ISBN:
Category : Automatic control
Languages : en
Pages : 44
Book Description
A Numerical Study of Supersonic Flow Past a Circular Cylinder
Author: Noel Andrés Modesto-Madera
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 70
Book Description
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 70
Book Description
Numerical Study of the Gas Flow in Nozzles and Supersonic Jets for Different Values of Specific Heats
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages :
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages :
Book Description
Numerical Study on Supersonic Internal Cavity Flows
Author: Yoko Takakura
Publisher:
ISBN:
Category :
Languages : en
Pages :
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages :
Book Description
Numerical Study of Unsteady Viscous Hypersonic Blunt Body Flows with an Impinging Shock
Author: Goetz H. Klopfer
Publisher:
ISBN:
Category : Aerodynamics, Hypersonic
Languages : en
Pages : 16
Book Description
Publisher:
ISBN:
Category : Aerodynamics, Hypersonic
Languages : en
Pages : 16
Book Description