Inviscid Supersonic Nonuniform Flows Over Sharp and Spherically Blunted Cones at Angle of Attack

Inviscid Supersonic Nonuniform Flows Over Sharp and Spherically Blunted Cones at Angle of Attack
Author: Roie R. Black
Publisher:
Total Pages: 0
Release: 1973
Genre: Aerodynamics, Supersonic
ISBN:

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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).

Inviscid Supersonic Nonuniform Flows Over Sharp and Spherically Blunted Cones at Angle of Attack. Volume II. Computer Program Descriptions and User's Guide

Inviscid Supersonic Nonuniform Flows Over Sharp and Spherically Blunted Cones at Angle of Attack. Volume II. Computer Program Descriptions and User's Guide
Author: Roie R. Balck
Publisher:
Total Pages: 145
Release: 1973
Genre:
ISBN:

Download Inviscid Supersonic Nonuniform Flows Over Sharp and Spherically Blunted Cones at Angle of Attack. Volume II. Computer Program Descriptions and User's Guide Book in PDF, Epub and Kindle

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).

Inviscid Supersonic Nonuniform Flows Over Sharp and Spherically Blunted Cones at Angle of Attack. Volume I. Engineering Report

Inviscid Supersonic Nonuniform Flows Over Sharp and Spherically Blunted Cones at Angle of Attack. Volume I. Engineering Report
Author: Roie R. Black
Publisher:
Total Pages: 115
Release: 1973
Genre:
ISBN:

Download Inviscid Supersonic Nonuniform Flows Over Sharp and Spherically Blunted Cones at Angle of Attack. Volume I. Engineering Report Book in PDF, Epub and Kindle

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).

Instability, Transition, and Turbulence

Instability, Transition, and Turbulence
Author: M.Y. Hussaini
Publisher: Springer Science & Business Media
Total Pages: 626
Release: 2012-12-06
Genre: Science
ISBN: 1461229561

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This volume contains the proceedings of the Workshop on In stability, Transition and Turbulence, sponsored by the Institute for Computer Applications in Science and Engineering (ICASE) and the NASA Langley Research Center (LaRC), during July 8 to August 2, 1991. This is the second workshop in the series on the subject. The first was held in 1989, and its proceedings were published by Springer-Verlag under the title "Instability and Transition" edited by M. Y. Hussaini and R. G. Voigt. The objectives of these work shops are to i) expose the academic community to current technologically im portant issues of transition and turbulence in shear flows over the entire speed range, ii) acquaint the academic community with the unique combination of theoretical, computational and experimental capabilities at LaRC and foster interaction with these capabilities, and iii) accelerate progress in elucidating the fundamental phenomena of transition and turbulence, leading to improved transition and turbulence modeling in design methodologies. The research areas covered in these proceedings include receptiv ity and roughness, nonlinear theories of transition, numerical simu lation of spatially evolving flows, modelling of transitional and fully turbulent flows as well as some experiments on instability and tran sition. In addition a one-day mini-symposium was held to discuss 1 recent and planned experiments on turbulent flow over a backward facing step.

Instability and Transition

Instability and Transition
Author: M.Y. Hussaini
Publisher: Springer Science & Business Media
Total Pages: 509
Release: 2012-12-06
Genre: Science
ISBN: 1461234328

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The ability to predict and control viscous flow phenomena is becoming increasingly important in modern industrial application. The Instability and Transition Workshop at Langley was extremely important in help§ ing the scientists community to access the state of knowledge in the area of transition from laminar to turbulent flow, to identify promising future areas of research and to build future interactions between researchers worldwide working in the areas of theoretical, experimental and computational fluid and aero dynamics. The set of two volume contains panel discussions and research contribution with the following objectives: (1) expose the academic community to current technologically important issues of instability and transitions in shear flows over the entire speed range, (2) acquaint the academic community with the unique combination of theoretical, computational and experimental capabilities at LaRC and foster interaction with these facilities. (3) review current state-of-the-art and propose future directions for instability and transition research, (4) accelerate progress in elucidating basic understanding of transition phenomena and in transferring this knowledge into improved design methodologies through improved transition modeling, and (5) establish mechanism for continued interaction.

Three-dimensional Inviscid Flow about Supersonic Blunt Cones at Angle of Attack

Three-dimensional Inviscid Flow about Supersonic Blunt Cones at Angle of Attack
Author: G. Moretti
Publisher:
Total Pages: 36
Release: 1968
Genre: Aerodynamics, Supersonic
ISBN:

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Comparisons are made between the cylindrical and polar coordinate system used in determining the three-dimensional shock layer flow over the nose region of a blunted supersonic vehicle. Jusfification for the development of a polar coordinate system is given and an outline for such development is presented. Results from the polar coordinate system are given as is the limiting useful range.

Inviscid Supersonic Nonuniform Flows Over Sharp and Spherically Blunted Cones at Angle of Attack

Inviscid Supersonic Nonuniform Flows Over Sharp and Spherically Blunted Cones at Angle of Attack
Author: Roie R. Black
Publisher:
Total Pages: 0
Release: 1973
Genre: Aerodynamics, Supersonic
ISBN:

Download Inviscid Supersonic Nonuniform Flows Over Sharp and Spherically Blunted Cones at Angle of Attack Book in PDF, Epub and Kindle

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).