Computation of Supersonic Flow over Flying Configurations

Computation of Supersonic Flow over Flying Configurations
Author: Adriana Nastase
Publsiher: Elsevier
Total Pages: 410
Release: 2010-07-07
ISBN 10: 9780080556994
ISBN 13: 008055699X
Language: EN, FR, DE, ES & NL

Computation of Supersonic Flow over Flying Configurations Book Review:

Computation of Supersonic Flow over Flying Configurations is a high-level aerospace reference book that will be useful for undergraduate and graduate students of engineering, applied mathematics and physics. The author provides solutions for three-dimensional compressible Navier-Stokes layer subsonic and supersonic flows. Computational work and experimental results show the real-world application of computational results Easy computation and visualization of inviscid and viscous aerodynamic characteristics of flying configurations Includes a fully optimized and integrated design for a proposed supersonic transport aircraft

Computation of Supersonic Flow over Flying Configurations

Computation of Supersonic Flow over Flying Configurations
Author: Anonim
Publsiher: Unknown
Total Pages: 329
Release: 2021
ISBN 10:
ISBN 13: OCLC:873984086
Language: EN, FR, DE, ES & NL

Computation of Supersonic Flow over Flying Configurations Book Review:

International Aerospace Abstracts

International Aerospace Abstracts
Author: Anonim
Publsiher: Unknown
Total Pages: 329
Release: 1996
ISBN 10:
ISBN 13: UOM:39015040314554
Language: EN, FR, DE, ES & NL

International Aerospace Abstracts Book Review:

Scientific and Technical Aerospace Reports

Scientific and Technical Aerospace Reports
Author: Anonim
Publsiher: Unknown
Total Pages: 329
Release: 1978
ISBN 10:
ISBN 13: UVA:X004872604
Language: EN, FR, DE, ES & NL

Scientific and Technical Aerospace Reports Book Review:

Aeronautical Engineering

Aeronautical Engineering
Author: Anonim
Publsiher: Unknown
Total Pages: 329
Release: 1993
ISBN 10:
ISBN 13: STANFORD:36105012119850
Language: EN, FR, DE, ES & NL

Aeronautical Engineering Book Review:

A selection of annotated references to unclassified reports and journal articles that were introduced into the NASA scientific and technical information system and announced in Scientific and technical aerospace reports (STAR) and International aerospace abstracts (IAA)

Special Course on Modern Theoretical and Experimental Approaches to Turbulent Flow Structure and Its Modelling

Special Course on Modern Theoretical and Experimental Approaches to Turbulent Flow Structure and Its Modelling
Author: Anonim
Publsiher: Unknown
Total Pages: 329
Release: 1987
ISBN 10:
ISBN 13: OSU:32435029442084
Language: EN, FR, DE, ES & NL

Special Course on Modern Theoretical and Experimental Approaches to Turbulent Flow Structure and Its Modelling Book Review:

The Finding Guide to AIAA Meeting Papers

The Finding Guide to AIAA Meeting Papers
Author: American Institute of Aeronautics and Astronautics. Technical Information Service
Publsiher: Unknown
Total Pages: 329
Release: 1990
ISBN 10:
ISBN 13: UOM:39015023876017
Language: EN, FR, DE, ES & NL

The Finding Guide to AIAA Meeting Papers Book Review:

AIAA Aerospace Sciences Meeting and Exhibit 42nd

AIAA Aerospace Sciences Meeting and Exhibit  42nd
Author: Anonim
Publsiher: Unknown
Total Pages: 329
Release: 2004
ISBN 10:
ISBN 13: PSU:000054739536
Language: EN, FR, DE, ES & NL

AIAA Aerospace Sciences Meeting and Exhibit 42nd Book Review:

NASA SP

NASA SP
Author: Anonim
Publsiher: Unknown
Total Pages: 329
Release: 1962
ISBN 10:
ISBN 13: MINN:30000002998767
Language: EN, FR, DE, ES & NL

NASA SP Book Review:

Government Reports Announcements Index

Government Reports Announcements   Index
Author: Anonim
Publsiher: Unknown
Total Pages: 329
Release: 1993
ISBN 10:
ISBN 13: MINN:31951P00246174E
Language: EN, FR, DE, ES & NL

Government Reports Announcements Index Book Review:

Physics Briefs

Physics Briefs
Author: Anonim
Publsiher: Unknown
Total Pages: 329
Release: 1986
ISBN 10:
ISBN 13: UOM:39015027835332
Language: EN, FR, DE, ES & NL

Physics Briefs Book Review:

Development of a computer code for calculating the steady super hypersonic inviscid flow around real configurations

Development of a computer code for calculating the steady super hypersonic inviscid flow around real configurations
Author: Frank Marconi,Manuel Salas,Larry Yaeger
Publsiher: Unknown
Total Pages: 92
Release: 1976
ISBN 10:
ISBN 13: UIUC:30112106770081
Language: EN, FR, DE, ES & NL

Development of a computer code for calculating the steady super hypersonic inviscid flow around real configurations Book Review:

Calculations of Inviscid Flow Over Shuttle like Vehicles at High Angles of Attack and Comparisons with Experimental Data

Calculations of Inviscid Flow Over Shuttle like Vehicles at High Angles of Attack and Comparisons with Experimental Data
Author: K. James Weilmuenster
Publsiher: Unknown
Total Pages: 86
Release: 1983
ISBN 10:
ISBN 13: UIUC:30112101594262
Language: EN, FR, DE, ES & NL

Calculations of Inviscid Flow Over Shuttle like Vehicles at High Angles of Attack and Comparisons with Experimental Data Book Review:

AIAA 27th Aerospace Sciences Meeting

AIAA 27th Aerospace Sciences Meeting
Author: Anonim
Publsiher: Unknown
Total Pages: 329
Release: 1989
ISBN 10:
ISBN 13: PSU:000016363601
Language: EN, FR, DE, ES & NL

AIAA 27th Aerospace Sciences Meeting Book Review:

Aeronautical Engineering A Cumulative Index to a Continuing Bibliography supplement 300

Aeronautical Engineering  A Cumulative Index to a Continuing Bibliography  supplement 300
Author: Anonim
Publsiher: Unknown
Total Pages: 673
Release: 1994
ISBN 10:
ISBN 13: NASA:31769000659378
Language: EN, FR, DE, ES & NL

Aeronautical Engineering A Cumulative Index to a Continuing Bibliography supplement 300 Book Review:

A Cumulative Index to a Continuing Bibliography on Aeronautical Engineering

A Cumulative Index to a Continuing Bibliography on Aeronautical Engineering
Author: Anonim
Publsiher: Unknown
Total Pages: 521
Release: 1986
ISBN 10:
ISBN 13: NASA:31769000659295
Language: EN, FR, DE, ES & NL

A Cumulative Index to a Continuing Bibliography on Aeronautical Engineering Book Review:

Computer program abstracts

Computer program abstracts
Author: United States. National Aeronautics and Space Administration. Scientific and Technical Information Office,Informatics Information Systems Company,United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch
Publsiher: Unknown
Total Pages: 329
Release: 1969
ISBN 10:
ISBN 13: UIUC:30112075696937
Language: EN, FR, DE, ES & NL

Computer program abstracts Book Review:

A Collection of Technical Papers

A Collection of Technical Papers
Author: Anonim
Publsiher: Unknown
Total Pages: 329
Release: 1976
ISBN 10:
ISBN 13: PSU:000011749066
Language: EN, FR, DE, ES & NL

A Collection of Technical Papers Book Review:

European Aerospace Science and Technology 1992 A Bibliography with Indexes

European Aerospace Science and Technology  1992  A Bibliography with Indexes
Author: Anonim
Publsiher: Unknown
Total Pages: 485
Release: 1993
ISBN 10:
ISBN 13: NASA:31769000660533
Language: EN, FR, DE, ES & NL

European Aerospace Science and Technology 1992 A Bibliography with Indexes Book Review:

Multigrid for Hypersonic Viscous Two and Three dimensional Flows

Multigrid for Hypersonic Viscous Two  and Three dimensional Flows
Author: Institute for Computer Applications in Science and Engineering,E. Turkel
Publsiher: Unknown
Total Pages: 24
Release: 1991
ISBN 10:
ISBN 13: NASA:31769000687221
Language: EN, FR, DE, ES & NL

Multigrid for Hypersonic Viscous Two and Three dimensional Flows Book Review:

We consider the use of a multigrid method with central differencing to solve the Navier Stokes equation for hypersonic flows. The time-dependent form of the equations is integrated with an explicit Runge-Kutta scheme accelerated by local time stepping and implicit residual smoothing. Variable coefficients are developed for the implicit process that remove the diffusion limit on the time step, producing significant improvement in convergence. A numerical dissipation formulation that provides good shock-capturing capability for hypersonic flow is presented. This formulation is shown to be a crucial aspect of the multigrid method. Solutions are given for two-dimensional viscous flow over a NACA 0012 airfoil and three-dimensional viscous flow over a blunt biconic.