Inviscid Supersonic Nonuniform Flows Over Sharp and Spherically Blunted Cones at Angle of Attack. Volume II. Computer Program Descriptions and User's Guide PDF Download
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Author: Roie R. Balck
Publisher:
ISBN:
Category :
Languages : en
Pages : 145
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Book Description
A system of six computer programs which may be arranged into several program packages for the purpose of solving inviscid flow fields over sharp and spherically blunted cones at angle of attack in both uniform and nonuniform supersonic free streams has been developed. These programs are written in standard FORTRAN 4 and are currently being run on the Virginia Polytechnic Inst. and State University IBM 370/155 computer. The six programs include a modified inverse blunt body solution program, a modified axisymmetric method of characteristics program, a modified three-dimensional method of characteristics program, two sharp cone zero and nonzero angle of attack uniform flow solution programs, and a master data input control program which reads input data and passes information to the other programs. (Modified author abstract).
Author: Roie R. Balck
Publisher:
ISBN:
Category :
Languages : en
Pages : 145
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Book Description
A system of six computer programs which may be arranged into several program packages for the purpose of solving inviscid flow fields over sharp and spherically blunted cones at angle of attack in both uniform and nonuniform supersonic free streams has been developed. These programs are written in standard FORTRAN 4 and are currently being run on the Virginia Polytechnic Inst. and State University IBM 370/155 computer. The six programs include a modified inverse blunt body solution program, a modified axisymmetric method of characteristics program, a modified three-dimensional method of characteristics program, two sharp cone zero and nonzero angle of attack uniform flow solution programs, and a master data input control program which reads input data and passes information to the other programs. (Modified author abstract).
Author: Roie R. Black
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 0
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Book Description
A system of six computer programs which may be arranged into several program packages for the purpose of solving inviscid flow fields over sharp and spherically blunted cones at angle of attack in both uniform and nonuniform supersonic free streams has been developed. These programs are written in standard FORTRAN 4 and are currently being run on the Virginia Polytechnic Inst. and State University IBM 370/155 computer. The six programs include a modified inverse blunt body solution program, a modified axisymmetric method of characteristics program, a modified three-dimensional method of characteristics program, two sharp cone zero and nonzero angle of attack uniform flow solution programs, and a master data input control program which reads input data and passes information to the other programs. (Modified author abstract).
Author: Michael C. Frieders
Publisher:
ISBN:
Category :
Languages : en
Pages : 169
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Book Description
Two fortran computer programs have been developed to solve the problem of laminar boundary layers on sharp and blunt cones at angle of attack to nonuniform free streams. An existing three-dimensional boundary layer program was modified to introduce nonuniform edge properties to the boundary layer on a sharp cone. A combination of axisymmetric and three-dimensional boundary layer programs was modified to solve the boundary layer on a blunt cone in nonuniform streams. The inviscid flow fields over blunt cones are predicted from blunt body and three-dimensional method of characteristics solutions. Conical flow field solutions are used over sharp cones in uniform streams, and three-dimensional method of characteristics solutions are used over sharp cones in nonuniform streams. (Modified author abstract).
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 960
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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.
Author: Michael C. Frieders
Publisher:
ISBN:
Category :
Languages : en
Pages : 258
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Book Description
Author: Roie R. Black
Publisher:
ISBN:
Category :
Languages : en
Pages : 115
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Book Description
A system of computer programs was developed to solve supersonic inviscid nonuniform flows over sharp and spherically blunted cones at angles of attack. For blunt cones the flow fields considered were axisymmetric wake flows situated so that flow in the subsonic nose region remained axisymmetric. For sharp cones both axisymmetric wake flows and two-dimensional shear flows were considered. The programs incorporate a modified inverse method for solving subsonic flow regions and modified axisymmetric and three-dimensional method of characteristics procedures for solving supersonic flow regions. (Modified author abstract).
Author: Wilbur L. Hankey
Publisher:
ISBN:
Category : Aerodynamics, Hypersonic
Languages : en
Pages : 20
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Book Description
This report reviews the progress over the last decade on separated flows conducted at these laboratories. Experimental investigations conducted in the hypersonic wind tunnels is discussed. Advancements are summarized in the theoretical area which cover the development of interacting boundary layers to the numerical computation of the complete Navier-Stokes equations.
Author:
Publisher:
ISBN:
Category : Computer programming
Languages : en
Pages : 240
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Book Description
Author: Roie R. Black
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 0
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Book Description
A system of computer programs was developed to solve supersonic inviscid nonuniform flows over sharp and spherically blunted cones at angles of attack. For blunt cones the flow fields considered were axisymmetric wake flows situated so that flow in the subsonic nose region remained axisymmetric. For sharp cones both axisymmetric wake flows and two-dimensional shear flows were considered. The programs incorporate a modified inverse method for solving subsonic flow regions and modified axisymmetric and three-dimensional method of characteristics procedures for solving supersonic flow regions. (Modified author abstract).
Author:
Publisher:
ISBN:
Category : Research
Languages : en
Pages : 1000
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Book Description
