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Author : Charles E. Wittliff
Publisher :
ISBN 13 :
Total Pages : 58 pages
Book Rating : 4.E/5 ( download)
Download or read book Shock Tube Driver Techniques and Attenuation Measurements written by Charles E. Wittliff and published by . This book was released on 1957 with total page 58 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Jim J. Jones
Publisher :
ISBN 13 :
Total Pages : 716 pages
Book Rating : 4.F/5 ( download)
Download or read book Experimental Investigation of Attenuation of Strong Shock Waves in a Shock Tube with Hydrogen and Helium as Driver Gases written by Jim J. Jones and published by . This book was released on 1957 with total page 716 pages. Available in PDF, EPUB and Kindle. Book excerpt: An experimental investigation has been made of the attenuation of strong shock waves in air in a shock tube. Time-history measurements were made of the static pressure at several stations in the wall of the tube. The internal diameter of the tube is 3.75 inches. shock-wave-velocity data were taken for a distance along the tube of about 120 feet.
Author : I. I. Glass
Publisher : [Toronto, Ont.] : University of Toronto Press
ISBN 13 :
Total Pages : 860 pages
Book Rating : 4.3/5 (91 download)
Download or read book Shock Tubes written by I. I. Glass and published by [Toronto, Ont.] : University of Toronto Press. This book was released on 1970 with total page 860 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author :
Publisher :
ISBN 13 :
Total Pages : 722 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 722 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : United States. Wright Air Development Division
Publisher :
ISBN 13 :
Total Pages : 1338 pages
Book Rating : 4.3/5 (91 download)
Download or read book WADC Technical Report written by United States. Wright Air Development Division and published by . This book was released on 1961 with total page 1338 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Aerospace Corporation
Publisher :
ISBN 13 :
Total Pages : 72 pages
Book Rating : 4.E/5 ( download)
Download or read book Shock Tube Test Time Limitation Due to Turbulent Wall Boundary Layer written by Aerospace Corporation and published by . This book was released on 1963 with total page 72 pages. Available in PDF, EPUB and Kindle. Book excerpt: Shock tube test time limitation due to the premature arrival of the contact surface is analytically investigated for wholly turbulent wall boundary layers. The results are compared with those for wholly laminar wall boundary layers. Working curves are presented for more accurate estimates of test time in specific cases. (Author) -- NTRL website.
Author :
Publisher :
ISBN 13 :
Total Pages : 550 pages
Book Rating : 4.:/5 (319 download)
Download or read book NASA Technical Report written by and published by . This book was released on 1966 with total page 550 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Wolfgang Merzkirch
Publisher :
ISBN 13 :
Total Pages : 6 pages
Book Rating : 4.:/5 (228 download)
Download or read book Measurement and Calculation of Shock Attenuation in a Channel with Perforated Walls written by Wolfgang Merzkirch and published by . This book was released on 1981 with total page 6 pages. Available in PDF, EPUB and Kindle. Book excerpt: The velocity of a shock wave generated in an air/air shock tube with perforated walls is measured by means of an optical Doppler schlieren technique. The attenuation of the shock is measured for perforation ratios varying between 0.1 and 0.5 and over a length of about 40 channel heights. Various numerical models are used to determine the shock attenuation, and these results are compared with the experimental data.
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 : 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 : F.R. Riddell
Publisher : Elsevier
ISBN 13 : 0323142621
Total Pages : 769 pages
Book Rating : 4.3/5 (231 download)
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.
Author : C. E. Wooldridge
Publisher :
ISBN 13 :
Total Pages : 49 pages
Book Rating : 4.:/5 (227 download)
Download or read book Measurements of Shock Wave Attenuation in Ducts with Large Length-to-Diameter Ratios written by C. E. Wooldridge and published by . This book was released on 1969 with total page 49 pages. Available in PDF, EPUB and Kindle. Book excerpt: An investigation was conducted to determine the magnitude of viscous attenuation of the shock front in smooth-walled tubes with a length-to-diameter (L/D) ratio of 600. The tests were carried out in a hydrogen driven shock tube of 0.485-inch inside diameter, with air and sulfur hexafluoride as the driven gases. The pressure in the driven section was held at 1 atmosphere for the tests ranging up to a Mach number of 8.9. It was reduced below 1 atmosphere at higher mach numbers in order to avoid heating. The incident shock produced a square pressure pulse. The initial shock Mach numbers were varied from about 3.5 to 15.7. The corresponding initial shock overpressure ratios varied from about 15 to 250. (Author).
Author : Robert L. Trimpi
Publisher :
ISBN 13 :
Total Pages : 68 pages
Book Rating : 4.:/5 (317 download)
Download or read book A Theoretical Investigation of Simulation in Expansion Tubes and Tunnels written by Robert L. Trimpi and published by . This book was released on 1966 with total page 68 pages. Available in PDF, EPUB and Kindle. Book excerpt: A preliminary theoretical analysis was conducted of expansion-tube and expansion-tunnel simulation whereby the postnormal shock stagnation conditions of a model were matched to those of flight for both a perfect gas and equilibrium real air. The selected simulation mode permitted large variations from flight conditions for the test-section ambient temperature and pressure but only a small excursion for ambient velocity or density. A brief treatment of the perfect-gas expansion tunnel with simulation demonstrated both gains and penalties in driver performance, depending on the Mach number, nozzle area ratio, driver gas, and simulation temperature ratio. A more exhaustive analysis of an equilibrium real-air expansion tube employing simulation with ambient-gas temperatures of 1000° and 2000°K was completed for equivalent flight velocities from 20,000 to 50,000 feet per second (6.096 to 15.24 km/sec) and altitudes from 100,000 to 300,000 feet (30..48 to 91.44 km). The primary advantages of simulation were found to be large increases in testing time, initial test-gas slug length, and velocity-altitude performance. The primary disadvantages were a small degree of test-section dissociation and an increased peak cycle dissociation for the highest flow velocities and altitudes. For equilibrium flow the gas state behind a shock wave was found to be closely simulated by all strong shock waves and to be well simulated even by weak waves with flow deflections as low as 30°
Author : Charles E. Treanor
Publisher : State University of New York Press
ISBN 13 : 1438405502
Total Pages : 908 pages
Book Rating : 4.4/5 (384 download)
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.
Author : United States. National Advisory Committee for Aeronautics
Publisher :
ISBN 13 :
Total Pages : 1146 pages
Book Rating : 4.E/5 ( download)
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 1957 with total page 1146 pages. Available in PDF, EPUB and Kindle. Book excerpt:
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 : S. P. Pfaff
Publisher :
ISBN 13 :
Total Pages : 30 pages
Book Rating : 4.3/5 (91 download)
Download or read book Measurement of Frequency Response of Pressure Gauges by a High-pressure Shock Tube Technique written by S. P. Pfaff and published by . This book was released on 1958 with total page 30 pages. Available in PDF, EPUB and Kindle. Book excerpt:
