Author: Lawrence Spradley
Publisher:
ISBN:
Category : Fluid mechanics
Languages : en
Pages : 212
Book Description
GIM Code User's Manual for the STAR-100 Computer
Author: Lawrence Spradley
Publisher:
ISBN:
Category : Fluid mechanics
Languages : en
Pages : 212
Book Description
Publisher:
ISBN:
Category : Fluid mechanics
Languages : en
Pages : 212
Book Description
Scientific and Technical Aerospace Reports
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1280
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1280
Book Description
Hyperbolic/parabolic Development for the GIM-STAR Code
Author: L. W. Spradley
Publisher:
ISBN:
Category : Boundary layer
Languages : en
Pages : 188
Book Description
low fields in supersonic inlet configurations were computed using the eliptic GIM code on the STAR computer. Spillage flow under the lower cowl was calculated to be 33% of the incoming stream. The shock/boundary layer interaction on the upper propulsive surface was computed including separation. All shocks produced by the flow system were captured. Linearized block implicit (LBI) schemes were examined to determine their application to the GIM code. Pure explicit methods have stability limitations and fully implicit schemes are inherently inefficient; however, LBI schemes show promise as an effective compromise. A quasiparabolic version of the GIM code was developed using elastical parabolized Navier-Stokes methods combined with quasitime relaxation. This scheme is referred to as quasiparabolic although it applies equally well to hyperbolic supersonic inviscid flows. Second order windward differences are used in the marching coordinate and either explicit or linear block implicit time relaxation can be incorporated. (NTRL site)
Publisher:
ISBN:
Category : Boundary layer
Languages : en
Pages : 188
Book Description
low fields in supersonic inlet configurations were computed using the eliptic GIM code on the STAR computer. Spillage flow under the lower cowl was calculated to be 33% of the incoming stream. The shock/boundary layer interaction on the upper propulsive surface was computed including separation. All shocks produced by the flow system were captured. Linearized block implicit (LBI) schemes were examined to determine their application to the GIM code. Pure explicit methods have stability limitations and fully implicit schemes are inherently inefficient; however, LBI schemes show promise as an effective compromise. A quasiparabolic version of the GIM code was developed using elastical parabolized Navier-Stokes methods combined with quasitime relaxation. This scheme is referred to as quasiparabolic although it applies equally well to hyperbolic supersonic inviscid flows. Second order windward differences are used in the marching coordinate and either explicit or linear block implicit time relaxation can be incorporated. (NTRL site)
Monthly Catalog of United States Government Publications
Author:
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1084
Book Description
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1084
Book Description
The Use of Interactive Graphic Displays for Interpretation of Surface Design Parameters
Author: Noel A. Talcott
Publisher:
ISBN:
Category : Aerodynamic heating
Languages : en
Pages : 42
Book Description
Publisher:
ISBN:
Category : Aerodynamic heating
Languages : en
Pages : 42
Book Description
Monthly Catalogue, United States Public Documents
Author:
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1094
Book Description
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1094
Book Description
The Use of Interpractive Graphic Displays for Interpretation of Surface Design Parameters
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 32
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 32
Book Description
The Aeronautical Journal
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 582
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 582
Book Description
Development of the General Interpolants Method for the CYBER 200 Series of Supercomputers
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 324
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 324
Book Description
NASA Technical Memorandum
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 694
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 694
Book Description