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Author : Eva Winkler
Publisher :
ISBN 13 :
Total Pages : 12 pages
Book Rating : 4.:/5 (977 download)
Download or read book NOL Hypersonic Tunnel No. 4 Results IV: High Supply Temperature Measurement and Control written by Eva Winkler and published by . This book was released on 1952 with total page 12 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : James E. Danberg
Publisher :
ISBN 13 :
Total Pages : 84 pages
Book Rating : 4.3/5 (91 download)
Download or read book NOL Hypersonic Tunnel No. 4 written by James E. Danberg and published by . This book was released on 1964 with total page 84 pages. Available in PDF, EPUB and Kindle. Book excerpt: NOL's Hypersonic Tunnel No. 4 is a continuous blow-down hypersonic tunnel designed for research and development testing of models, instrumentation, and wind tunnel components. It can operate at Mach numbers from 5 to 10 with supply pressures up to 52 atmospheres and supply temperatures up to 1700 R. This report summarizes the pertinent aerodynamic design criteria and operating experience compiled during its first eleven years of operation. Included are descriptions of the major components and their performance along with the flight simulation capability of the facility and a bibliography of previously published reports. (Author).
Author : P. Wegener
Publisher :
ISBN 13 :
Total Pages : 66 pages
Book Rating : 4.:/5 (227 download)
Download or read book NOL Hyperballistics Tunnel No. 4 Results I: Air Liquefaction written by P. Wegener and published by . This book was released on 1951 with total page 66 pages. Available in PDF, EPUB and Kindle. Book excerpt: Since the presence of condensed air in a hypersonic wind tunnel can make the operation of the tunnel difficult, and since liquefaction can occur when the temperature and pressure in the test section are below the condensation values, an investigation was carried out on the liquefaction of air in a hypersonic wind tunnel. The tunnel used was built to operate at Mach numbers up to 11. The liquefaction was investigated under conditions in which the temperature and pressure of the supply air could be varied. It was found that air, unlike water vapor, does not supersaturate and heating of the supply air is required for satisfactory operation of a hypersonic wind tunnel. Experimental measurements show that a portion of the air condenses at or shortly after it reaches the predicted conditions for equilibrium-saturation in the nozzle. Since the presence of liquefaction may affect standard methods of measuring the Mach number of the flow in the tunnel, the response of these standard methods to liquefaction was examined. It was found that pitot-tube determinations of Mach number are relatively insensitive to air liquefaction whereas determinations using static pressures and shock-wave angles that are produced by slender bodies vary with the amount of air condensation. By maintaining a high temperature in the supply air the various standard methods for measuring the Mach number were found to give consistent Mach number data.
Author :
Publisher :
ISBN 13 :
Total Pages : 466 pages
Book Rating : 4.3/5 (243 download)
Download or read book U.S. Government Research Reports written by and published by . This book was released on 1956 with total page 466 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Defense Documentation Center (U.S.)
Publisher :
ISBN 13 :
Total Pages : 922 pages
Book Rating : 4.3/5 (91 download)
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:
Author :
Publisher :
ISBN 13 :
Total Pages : 1058 pages
Book Rating : 4.3/5 (91 download)
Download or read book The Texas Journal of Science written by and published by . This book was released on 1957 with total page 1058 pages. Available in PDF, EPUB and Kindle. Book excerpt: Includes the proceedings and transactions of the Academy.
Author : Harris M. Schurmeier
Publisher :
ISBN 13 :
Total Pages : 304 pages
Book Rating : 4.3/5 (91 download)
Download or read book Design and Operation of a Continuous-flow Hypersonic Wind Tunnel Using a Two-dimensional Nozzle written by Harris M. Schurmeier and published by . This book was released on 1959 with total page 304 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : California Institute of Technology. Graduate Aeronautical Laboratories
Publisher :
ISBN 13 :
Total Pages : 140 pages
Book Rating : 4.3/5 (91 download)
Download or read book Hypersonic Research Project written by California Institute of Technology. Graduate Aeronautical Laboratories and published by . This book was released on with total page 140 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : James E. Danberg
Publisher :
ISBN 13 :
Total Pages : 1 pages
Book Rating : 4.:/5 (227 download)
Download or read book NOL HYPERSONIC TUNNEL written by James E. Danberg and published by . This book was released on 1964 with total page 1 pages. Available in PDF, EPUB and Kindle. Book excerpt: NOL's Hypersonic Tunnel No. 4 is a continuous blow-down hypersonic tunnel designed for research and development testing of models, instrumentation, and wind tunnel components. It can operate at Mach numbers from 5 to 10 with supply pressures up to 52 atmospheres and supply temperatures up to 1700 R. This report summarizes the pertinent aerodynamic design criteria and operating experience compiled during its first eleven years of operation. Included are descriptions of the major components and their performance along with the flight simulation capability of the facility and a bibliography of previously published reports. (Author).
Author : Frank P. Baltakis
Publisher :
ISBN 13 :
Total Pages : 146 pages
Book Rating : 4.3/5 (91 download)
Download or read book Performance Capability of the NOL Hypersonic Tunnel written by Frank P. Baltakis and published by . This book was released on 1968 with total page 146 pages. Available in PDF, EPUB and Kindle. Book excerpt: The report summarizes the performance capability data of the U.S. Naval Ordnance Laboratory's Hypersonic Tunnel. The report includes a brief description of the facility, overall performance capability data, nozzle calibration data, and some nozzle boundary-layer thickness and temperature variation data. The nozzle aerodynamic design method is indicated and its adequacy in the range of the supply and test flow conditions of the Hypersonic Tunnel is briefly discussed. (Author).
Author : L. L. LICCINI
Publisher :
ISBN 13 :
Total Pages : 23 pages
Book Rating : 4.:/5 (227 download)
Download or read book Nol Hypersonic Tunnel No. 4 Results Viii: Development and Calibration of Mass Flow Probes in Hypersonic Flow written by L. L. LICCINI and published by . This book was released on 1955 with total page 23 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : North Atlantic Treaty Organization. Advisory Group for Aeronautical Research and Development
Publisher :
ISBN 13 :
Total Pages : 458 pages
Book Rating : 4.3/5 (243 download)
Download or read book Papers Presented at the Meeting of the Wind Tunnel and Model Testing Panel written by North Atlantic Treaty Organization. Advisory Group for Aeronautical Research and Development and published by . This book was released on 1954 with total page 458 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : E. M. Winkler
Publisher :
ISBN 13 :
Total Pages : 0 pages
Book Rating : 4.:/5 (977 download)
Download or read book NOL Hypersonic Tunnel No. 4 Results VI written by E. M. Winkler and published by . This book was released on 1954 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt:
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Author : North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development
Publisher :
ISBN 13 :
Total Pages : 1120 pages
Book Rating : 4.3/5 (91 download)
Download or read book AG [document] written by North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development and published by . This book was released on 1954 with total page 1120 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author :
Publisher :
ISBN 13 :
Total Pages : 40 pages
Book Rating : 4.:/5 (227 download)
Download or read book NOL HYPERSONIC TUNNEL NO. 4 - RESULTS VI: - EXPERIMENTAL AND THEORETICAL INVESTIGATION OF THE BOUNDARY LAYER AND HEAT TRANSFER CHARACTERISTICS OF A COOLED HYPERSONIC WEDGE NOZZLE AT A MACH NUMBER OF 5.5 written by and published by . This book was released on 1954 with total page 40 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : P. Wegener
Publisher :
ISBN 13 :
Total Pages : pages
Book Rating : 4.:/5 (11 download)
Download or read book NOL Hypersonic Tunnel No. 4 Results 5 written by P. Wegener and published by . This book was released on 1955 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : North Atlantic Treaty Organization. Advisory Group for Aeronautical Research and Development
Publisher :
ISBN 13 :
Total Pages : 674 pages
Book Rating : 4.:/5 (43 download)
Download or read book Papers written by North Atlantic Treaty Organization. Advisory Group for Aeronautical Research and Development and published by . This book was released on 1954 with total page 674 pages. Available in PDF, EPUB and Kindle. Book excerpt:
