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The Shock Tube As An Instrument For The Investigation Of Transonic And Supersonic Flow Patterns
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Book Synopsis The Shock Tube as an Instrument for the Investigation of Transonic and Supersonic Flow Patterns by : Frederick William Geiger
Download or read book The Shock Tube as an Instrument for the Investigation of Transonic and Supersonic Flow Patterns written by Frederick William Geiger and published by . This book was released on 1949 with total page 216 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis The Shock Tube as an Instrument for the Investigation of Transonic and Supersonic Flow Patterns by : F. W. Geiger
Download or read book The Shock Tube as an Instrument for the Investigation of Transonic and Supersonic Flow Patterns written by F. W. Geiger and published by . This book was released on 1981 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Application of Shock Tubes to Transonic Airfoil Testing at High Reynolds Numbers by :
Download or read book Application of Shock Tubes to Transonic Airfoil Testing at High Reynolds Numbers written by and published by . This book was released on 1978 with total page 78 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book NASA Technical Paper written by and published by . This book was released on 1978 with total page 76 pages. Available in PDF, EPUB and Kindle. Book excerpt:
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:
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:
Book Synopsis Handbook of Supersonic Aerodynamics by : I. I. Glass
Download or read book Handbook of Supersonic Aerodynamics written by I. I. Glass and published by . This book was released on 1959 with total page 642 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Handbook of Supersonic Aerodynamics by : Johns Hopkins University. Applied Physics Laboratory, Silver Spring, Md
Download or read book Handbook of Supersonic Aerodynamics written by Johns Hopkins University. Applied Physics Laboratory, Silver Spring, Md and published by . This book was released on 1950 with total page 642 pages. Available in PDF, EPUB and Kindle. Book excerpt:
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.
Book Synopsis ON THE SHOCK TUBE AS A TOOL FOR THE INVESTIGATION OF FLOW PHENOMENA. by : FREDERICK WILLIAM GEIGER
Download or read book ON THE SHOCK TUBE AS A TOOL FOR THE INVESTIGATION OF FLOW PHENOMENA. written by FREDERICK WILLIAM GEIGER and published by . This book was released on 1950 with total page 348 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis The Use of the Shock Tube in the Production of Uniform Fields of Transonic and Supersonic Flow by : Charles William Mautz
Download or read book The Use of the Shock Tube in the Production of Uniform Fields of Transonic and Supersonic Flow written by Charles William Mautz and published by . This book was released on 1949 with total page 276 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author :United States. National Aeronautics and Space Administration. Scientific and Technical Information Office Publisher : ISBN 13 : Total Pages :76 pages Book Rating :4.:/5 (31 download)
Book Synopsis Application of Shock Tubes to Transonic Airfoil Testing at High Reynolds Number by : United States. National Aeronautics and Space Administration. Scientific and Technical Information Office
Download or read book Application of Shock Tubes to Transonic Airfoil Testing at High Reynolds Number written by United States. National Aeronautics and Space Administration. Scientific and Technical Information Office and published by . This book was released on 1978 with total page 76 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book NACA Research Memorandum written by and published by . This book was released on 1951 with total page 38 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Applied Mechanics Reviews written by and published by . This book was released on 1968 with total page 700 pages. Available in PDF, EPUB and Kindle. Book excerpt:
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 48 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis The Use of Real Gases in a Shock Tube by : Russell Earl Duff
Download or read book The Use of Real Gases in a Shock Tube written by Russell Earl Duff and published by . This book was released on 1951 with total page 290 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis A SHOCK TUBE FOR PRODUCING SUBSONIC, TRANSONIC, AND SUPERSONIC FLOWS FOR AERODYNAMIC TESTING. by :
Download or read book A SHOCK TUBE FOR PRODUCING SUBSONIC, TRANSONIC, AND SUPERSONIC FLOWS FOR AERODYNAMIC TESTING. written by and published by . This book was released on 1963 with total page 24 pages. Available in PDF, EPUB and Kindle. Book excerpt: A shock tube is proposed in which the flow conditions between the shock wave and advancing interface are expected to range from low subsonic to moderate supersonic speeds. Furthermore, testing times of 10 msec or more are predicted, a time quite adequate for aerodynamic force measurements. The driven section in the proposed facility is large enough to accommodate large scale models. To test the feasibility of the proposed tube, a shock tube was assembled using a surplus 7-foot diameter vacuum tank as a driven section and 12-in. flanged pipe for the driver. A series of tests were performed to determine shock formation time and experimental testing time. The results of thest tests are reported.
