A Theory for Predicting the Flow of Real Gases in Shock Tubes with Experimental Verification

Download A Theory for Predicting the Flow of Real Gases in Shock Tubes with Experimental Verification PDF Online Free

Author :
Publisher :
ISBN 13 :
Total Pages : 674 pages
Book Rating : 4.F/5 ( download)

DOWNLOAD NOW!


Book Synopsis A Theory for Predicting the Flow of Real Gases in Shock Tubes with Experimental Verification by : Robert L. Trimpi

Download or read book A Theory for Predicting the Flow of Real Gases in Shock Tubes with Experimental Verification written by Robert L. Trimpi and published by . This book was released on 1955 with total page 674 pages. Available in PDF, EPUB and Kindle. Book excerpt: The nonlinear characteristic differential equations applicable to a quasi-one-dimensional unsteady channel flow with friction and heat transfer are linearized and integrated in functional form for the particular study of small perturbations from ideal shock-tube flows. If the equivalence of unsteady- and steady-flow boundary layers is assumed, the problem of determining the perturbation in the unsteady flow reduces to an evaluation of the drag of a flat plate in the equivalent steady flow.

Technical Note

Download Technical Note PDF Online Free

Author :
Publisher :
ISBN 13 :
Total Pages : 468 pages
Book Rating : 4.:/5 (31 download)

DOWNLOAD NOW!


Book Synopsis Technical Note by :

Download or read book Technical Note written by and published by . This book was released on 1955 with total page 468 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Technical Note - National Advisory Committee for Aeronautics

Download Technical Note - National Advisory Committee for Aeronautics PDF Online Free

Author :
Publisher :
ISBN 13 :
Total Pages : 970 pages
Book Rating : 4.E/5 ( download)

DOWNLOAD NOW!


Book Synopsis Technical Note - National Advisory Committee for Aeronautics by : United States. National Advisory Committee for Aeronautics

Download or read book Technical Note - National Advisory Committee for Aeronautics written by United States. National Advisory Committee for Aeronautics and published by . This book was released on 1955 with total page 970 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Shock Tubes and Waves

Download Shock Tubes and Waves PDF Online Free

Author :
Publisher : State University of New York Press
ISBN 13 : 1438405502
Total Pages : 908 pages
Book Rating : 4.4/5 (384 download)

DOWNLOAD NOW!


Book Synopsis Shock Tubes and Waves by : Charles E. Treanor

Download or read book Shock Tubes and Waves written by Charles E. Treanor and published by State University of New York Press. This book was released on 1982-06-30 with total page 908 pages. Available in PDF, EPUB and Kindle. Book excerpt: Sponsored by the U.S. Air Force Office of Scientific Research, this conference was held in Niagara Falls on July 6–9, 1981. This book includes material on the following topics: instrumentation and diagnostics, shock tube facilities and techniques, gas dynamic experiments, heat transfer and real gas effects, boundary layers, shock structure, shock propagation, laser and spectral optical studies, chem and kinetics, relaxation and excitation, ionization, dusty gases, two-phase flow and condensation, shock waves in the environment and energy, and energy-related processes. The book contains a total of 98 papers by well-known specialists.

A Nonlinear Theory for Predicting the Effects of Unsteady Laminar, Turbulent, Or Transitional Boundary Layers on the Attenuation of Shock Waves in a Shock Tube with Experimental Comparison

Download A Nonlinear Theory for Predicting the Effects of Unsteady Laminar, Turbulent, Or Transitional Boundary Layers on the Attenuation of Shock Waves in a Shock Tube with Experimental Comparison PDF Online Free

Author :
Publisher :
ISBN 13 :
Total Pages : 70 pages
Book Rating : 4.:/5 (317 download)

DOWNLOAD NOW!


Book Synopsis A Nonlinear Theory for Predicting the Effects of Unsteady Laminar, Turbulent, Or Transitional Boundary Layers on the Attenuation of Shock Waves in a Shock Tube with Experimental Comparison by : Robert L. Trimpi

Download or read book A Nonlinear Theory for Predicting the Effects of Unsteady Laminar, Turbulent, Or Transitional Boundary Layers on the Attenuation of Shock Waves in a Shock Tube with Experimental Comparison written by Robert L. Trimpi and published by . This book was released on 1961 with total page 70 pages. Available in PDF, EPUB and Kindle. Book excerpt: The linearized attenuation theory of NACA Technical Note 3375 is modified in the following manner: (a) an unsteady compressible local skin-friction coefficient is employed rather than the equivalent steady-flow incompressible coefficient; (b) a nonlinear approach is used to permit application of the theory to large attenuations; and (c) transition effects are considered. Curves are presented for predicting attenuation for shock pressure ratios up to 20 and a range of shock-tube Reynolds numbers. Comparison of theory and experimental data for shock-wave strengths between 1.5 and 10 over a wide range of Reynolds numbers shows good agreement with the nonlinear theory evaluated for a transition Reynolds number of 2.5 x 106

U.S. Government Research Reports

Download U.S. Government Research Reports PDF Online Free

Author :
Publisher :
ISBN 13 :
Total Pages : 298 pages
Book Rating : 4.3/5 (243 download)

DOWNLOAD NOW!


Book Synopsis U.S. Government Research Reports by :

Download or read book U.S. Government Research Reports written by and published by . This book was released on 1955 with total page 298 pages. Available in PDF, EPUB and Kindle. Book excerpt:

A Selected Listing of NASA Scientific and Technical Reports for ...

Download A Selected Listing of NASA Scientific and Technical Reports for ... PDF Online Free

Author :
Publisher :
ISBN 13 :
Total Pages : 818 pages
Book Rating : 4.X/5 (4 download)

DOWNLOAD NOW!


Book Synopsis A Selected Listing of NASA Scientific and Technical Reports for ... by :

Download or read book A Selected Listing of NASA Scientific and Technical Reports for ... written by and published by . This book was released on 1954 with total page 818 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Index of NACA Technical Publications

Download Index of NACA Technical Publications PDF Online Free

Author :
Publisher :
ISBN 13 :
Total Pages : 1338 pages
Book Rating : 4.3/5 (126 download)

DOWNLOAD NOW!


Book Synopsis Index of NACA Technical Publications by : United States. National Advisory Committee for Aeronautics

Download or read book Index of NACA Technical Publications written by United States. National Advisory Committee for Aeronautics and published by . This book was released on 1955 with total page 1338 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Subject Index to Unclassified ASTIA Documents

Download Subject Index to Unclassified ASTIA Documents PDF Online Free

Author :
Publisher :
ISBN 13 :
Total Pages : 922 pages
Book Rating : 4.3/5 (91 download)

DOWNLOAD NOW!


Book Synopsis Subject Index to Unclassified ASTIA Documents by : Defense Documentation Center (U.S.)

Download or read book Subject Index to Unclassified ASTIA Documents written by Defense Documentation Center (U.S.) and published by . This book was released on 1960 with total page 922 pages. Available in PDF, EPUB and Kindle. Book excerpt:

NASA Technical Report

Download NASA Technical Report PDF Online Free

Author :
Publisher :
ISBN 13 :
Total Pages : 822 pages
Book Rating : 4.3/5 (91 download)

DOWNLOAD NOW!


Book Synopsis NASA Technical Report by : United States. National Aeronautics and Space Administration

Download or read book NASA Technical Report written by United States. National Aeronautics and Space Administration and published by . This book was released on 1972 with total page 822 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Fundamental Data Obtained from Shock-tube Experiments

Download Fundamental Data Obtained from Shock-tube Experiments PDF Online Free

Author :
Publisher :
ISBN 13 :
Total Pages : 436 pages
Book Rating : 4.:/5 (318 download)

DOWNLOAD NOW!


Book Synopsis Fundamental Data Obtained from Shock-tube Experiments by : Antonio Ferri

Download or read book Fundamental Data Obtained from Shock-tube Experiments written by Antonio Ferri and published by . This book was released on 1961 with total page 436 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Catalog of Technical Reports

Download Catalog of Technical Reports PDF Online Free

Author :
Publisher :
ISBN 13 :
Total Pages : 850 pages
Book Rating : 4.:/5 (31 download)

DOWNLOAD NOW!


Book Synopsis Catalog of Technical Reports by : United States. Dept. of Commerce. Office of Technical Services

Download or read book Catalog of Technical Reports written by United States. Dept. of Commerce. Office of Technical Services and published by . This book was released on with total page 850 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Annual Report - National Advisory Committee for Aeronautics

Download Annual Report - National Advisory Committee for Aeronautics PDF Online Free

Author :
Publisher :
ISBN 13 :
Total Pages : pages
Book Rating : 4.F/5 ( download)

DOWNLOAD NOW!


Book Synopsis Annual Report - National Advisory Committee for Aeronautics by : United States. National Advisory Committee for Aeronautics

Download or read book Annual Report - National Advisory Committee for Aeronautics written by United States. National Advisory Committee for Aeronautics and published by . This book was released on 1957 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt: Includes the Committee's Technical reports no. 1-1058, reprinted in v. 1-37.

Test Time in Low Pressure Shock Tubes

Download Test Time in Low Pressure Shock Tubes PDF Online Free

Author :
Publisher :
ISBN 13 :
Total Pages : 86 pages
Book Rating : 4.E/5 ( download)

DOWNLOAD NOW!


Book Synopsis Test Time in Low Pressure Shock Tubes by : Aerospace Corporation

Download or read book Test Time in Low Pressure Shock Tubes written by Aerospace Corporation and published by . This book was released on 1962 with total page 86 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Report

Download Report PDF Online Free

Author :
Publisher :
ISBN 13 :
Total Pages : 524 pages
Book Rating : 4.:/5 (31 download)

DOWNLOAD NOW!


Book Synopsis Report by :

Download or read book Report written by and published by . This book was released on 1953 with total page 524 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Annual Report

Download Annual Report PDF Online Free

Author :
Publisher :
ISBN 13 :
Total Pages : 534 pages
Book Rating : 4.:/5 (319 download)

DOWNLOAD NOW!


Book Synopsis Annual Report by : United States. National Advisory Committee for Aeronautics

Download or read book Annual Report written by United States. National Advisory Committee for Aeronautics and published by . This book was released on 1953 with total page 534 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Hypersonic Flow Research

Download Hypersonic Flow Research PDF Online Free

Author :
Publisher : Elsevier
ISBN 13 : 0323142621
Total Pages : 769 pages
Book Rating : 4.3/5 (231 download)

DOWNLOAD NOW!


Book Synopsis Hypersonic Flow Research by : F.R. Riddell

Download or read book Hypersonic Flow Research written by F.R. Riddell and published by Elsevier. This book was released on 2012-12-02 with total page 769 pages. Available in PDF, EPUB and Kindle. Book excerpt: Progress in Astronautics and Rocketry, Volume 7: Hypersonic Flow Research compiles papers presented at a conference on hypersonics held at the Massachusetts Institute of Technology in August 1961. This book discusses the low Reynolds number effects, chemical kinetics effects, inviscid flow calculations, and experimental techniques relating to the problems in acquiring an understanding of hypersonic flow. The structure and composition of hypersonic wakes with attendant complex chemical kinetic effects is only briefly mentioned. This text consists of five parts. Parts A to C comprise of theoretical papers on the problems of calculating flow fields at hypersonic speeds. The experimental techniques that are of immediate practical interest in view of the difficulty of flight testing are discussed in Parts D and E. This publication is beneficial to engineers involved in advanced design problems.