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Author : Herbert S. Glick
Publisher :
ISBN 13 :
Total Pages : 172 pages
Book Rating : 4.3/5 (91 download)
Download or read book Flow Phenomena in Starting a Hypersonic Shock Tunnel written by Herbert S. Glick and published by . This book was released on 1955 with total page 172 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : John Gordon Hall
Publisher :
ISBN 13 :
Total Pages : 370 pages
Book Rating : 4.3/5 (91 download)
Download or read book Fundamental Phenomena in Hypersonic Flow written by John Gordon Hall and published by . This book was released on 1966 with total page 370 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Wilbur C. Nelson
Publisher : Elsevier
ISBN 13 : 1483223310
Total Pages : 801 pages
Book Rating : 4.4/5 (832 download)
Download or read book The High Temperature Aspects of Hypersonic Flow written by Wilbur C. Nelson and published by Elsevier. This book was released on 2014-12-02 with total page 801 pages. Available in PDF, EPUB and Kindle. Book excerpt: The High Temperature Aspects of Hypersonic Flow is a record of the proceedings of the AGARD-NATO Specialists' Meeting, held at the Technical Centre for Experimental Aerodynamics, Rhode-Saint-Genese, Belgium in April 1962. The book contains the papers presented during the meeting that tackled a broad range of topics in the aspects of hypersonic flow. The subjects covered during the meeting include pressure measurements, interference effects, the use of wind tunnels in aircraft development testing, high temperature gas characteristics, boundary layer research, stability and control and the use of rocket vehicles in flight research. Aerospace engineers and aeronautical engineers will find the book invaluable.
Author : Michael H. Sherman
Publisher :
ISBN 13 :
Total Pages : 0 pages
Book Rating : 4.:/5 (227 download)
Download or read book An Investigation Into the Use of an Existing Shock Tube as a Driver for a Hypersonic Shock Tunnel written by Michael H. Sherman and published by . This book was released on 1989 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt: This thesis describes experiments carried out using an existing tube alone, and with the tube connected to two-dimensional wedge nozzle. The range of maximum duration of steady reflected pressure from 3.5 to 5 milliseconds was achieved through tailored operation for incident shock strengths of 3.4 and 2.0, using pure Helium and a 70% Helium/30% Nitrogen mixture as the driver gas respectfully. Spark and continuous light shadowgraph techniques were attempted using an optical window at the Mach 4.3 location. Results demonstrated that the short duration flow phenomena in a shock tunnel can be recorded successfully using existing equipment. Calculations showed that the addition of a Mach 10 nozzle and 15 cu m (6' diameter x 15' long) dump chamber would provide a useful hypersonic facility for instruction and research. (KR).
Author : Johns Hopkins University. Applied Physics Laboratory, Silver Spring, Md
Publisher :
ISBN 13 :
Total Pages : 642 pages
Book Rating : 4.:/5 (31 download)
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:
Author : Robert L. Trimpi
Publisher :
ISBN 13 :
Total Pages : 116 pages
Book Rating : 4.:/5 (317 download)
Download or read book A Perfect-gas Analysis of the Expansion Tunnel written by Robert L. Trimpi and published by . This book was released on 1965 with total page 116 pages. Available in PDF, EPUB and Kindle. Book excerpt: A perfect-gas analysis is presented for an apparatus consisting of a basic expansion tube at the downstream end of which a nozzle has been added. The resultant tube at the downstream end of which a nozzle has been added. The resultant apparatus, named the expansion tunnel, is shown to have the following advantages when compared with the basic expansion tube: increased testing time, larger initial test-gas slug length, higher efficiency, and reduced secondary-diaphgram bursting problems. Principal disadvantages are requirement of an additional nozzle, and the requirement disadvantages are requirement of an additional nozzle, and the requirement of a larger ratio between maximum and minimum pressures in an operating cycle. Authors conclude inherent advantages more than compensate for disadvantages.
Author : I. I. Glass
Publisher :
ISBN 13 :
Total Pages : 642 pages
Book Rating : 4.3/5 (91 download)
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:
Author :
Publisher :
ISBN 13 :
Total Pages : 574 pages
Book Rating : 4.:/5 (319 download)
Download or read book NASA Technical Note written by and published by . This book was released on 1975 with total page 574 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Cornell Aeronautical Laboratory
Publisher :
ISBN 13 :
Total Pages : 320 pages
Book Rating : 4.E/5 ( download)
Download or read book Study of High-density Hypervelocity Flows and Similitudes written by Cornell Aeronautical Laboratory and published by . This book was released on 1967 with total page 320 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Wallace Hayes
Publisher : Elsevier
ISBN 13 : 032314876X
Total Pages : 481 pages
Book Rating : 4.3/5 (231 download)
Download or read book Hypersonic Flow Theory written by Wallace Hayes and published by Elsevier. This book was released on 2012-12-02 with total page 481 pages. Available in PDF, EPUB and Kindle. Book excerpt: Hypersonic Flow Theory presents the fundamentals of fluid mechanics, focusing on the hypersonic flow theory and approaches in theoretical aerodynamics. This book discusses the assumptions underlying hypersonic flow theory, unified supersonic-hypersonic similitude, two-dimensional and axisymmetric bodies, and circular cylinder. The constant-streamtube-area approximation, streamtube-continuity methods, and tangent-wedge and tangent-cone are also deliberated. This text likewise covers the similar laminar boundary layer solutions, bluntness induced interactions on slender bodies, and free molecule transfer theory. The dynamics of hypersonic flight or hypersonic wing theory, magnetohydrodynamic theory, or any developments involving treatment of the Boltzmann equation are not included. This publication is intended for hypersonic aerodynamicists, students, and researchers conducting work on the hypersonic flow phenomena.
Author : Charles E. Wittliff
Publisher :
ISBN 13 :
Total Pages : 118 pages
Book Rating : 4.E/5 ( download)
Download or read book Hypersonic Research in the Shock Tunnel written by Charles E. Wittliff and published by . This book was released on 1960 with total page 118 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author :
Publisher :
ISBN 13 :
Total Pages : 662 pages
Book Rating : 4.:/5 (319 download)
Download or read book NASA Technical Report written by and published by . This book was released on 1965 with total page 662 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Charles Edward Smith (Jr.)
Publisher :
ISBN 13 :
Total Pages : 130 pages
Book Rating : 4.F/5 ( download)
Download or read book An Analytic Study of the Starting Process in a Hypersonic Nozzle written by Charles Edward Smith (Jr.) and published by . This book was released on 1962 with total page 130 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : R. J. Vidal
Publisher :
ISBN 13 :
Total Pages : 54 pages
Book Rating : 4.:/5 (227 download)
Download or read book High Temperature Phenomena in Hypersonic Flows written by R. J. Vidal and published by . This book was released on 1964 with total page 54 pages. Available in PDF, EPUB and Kindle. Book excerpt: The report summarizes the results of a program of research on high temperature phenomena in hypersonic flows. The topics included in the program are shock tunnel studies of air flows over slender cones, theoretical and experimental investigations of nonequilibrium inviscid air flows, and studies of surface catalysis in nonequilibrium flows. The main results in each of these studies are reviewed. (Author).
Author :
Publisher :
ISBN 13 :
Total Pages : 52 pages
Book Rating : 4.3/5 (91 download)
Download or read book U.S. Government Research Reports written by and published by . This book was released on 1955 with total page 52 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Irving Israel Glass
Publisher : University of Toronto Press
ISBN 13 : 1487597584
Total Pages : 852 pages
Book Rating : 4.4/5 (875 download)
Download or read book Shock Tubes written by Irving Israel Glass and published by University of Toronto Press. This book was released on 1970-12-15 with total page 852 pages. Available in PDF, EPUB and Kindle. Book excerpt: This volume contains the proceedings of a symposium held at the University of Toronto in June 1969. The symposium consisted of six sessions; each containing an invited paper, followed by six contributed papers reporting on recent, relevant research and development. The topics are: a review of research problems in basic shock tube flows and the possibilities for the shock tube in the future; driving techniques; explosive drivers; theoretical and experimental research in electromagnetic shock tubes; chemical kinetics and spectroscopy; and a review of shock tube diagnostics, instrumentation and fundamental data as well as the measurement of physical quantities.
Author : Wallace D. Hayes
Publisher : Courier Corporation
ISBN 13 : 0486160483
Total Pages : 628 pages
Book Rating : 4.4/5 (861 download)
Download or read book Hypersonic Inviscid Flow written by Wallace D. Hayes and published by Courier Corporation. This book was released on 2012-07-13 with total page 628 pages. Available in PDF, EPUB and Kindle. Book excerpt: Unified, self-contained view of nonequilibrium effects, body geometries, and similitudes available in hypersonic flow and thin shock layer; appropriate for graduate-level courses in hypersonic flow theory. 1966 edition.
