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Nol Hypersonic Tunnel No 4
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Book Synopsis NOL Hypersonic Tunnel No. 4 by : James E. Danberg
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).
Book Synopsis NOL HYPERSONIC TUNNEL NO. 4, RESULTS 7: EXPERIMENTAL INVESTIGATION OF TURBULENT BOUNDARY LAYERS IN HYPERSONIC FLOW. by :
Download or read book NOL HYPERSONIC TUNNEL NO. 4, RESULTS 7: EXPERIMENTAL INVESTIGATION OF TURBULENT BOUNDARY LAYERS IN HYPERSONIC FLOW. written by and published by . This book was released on 1955 with total page 68 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis NOL HYPERSONIC TUNNEL by : James E. Danberg
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).
Book Synopsis NOL Hypersonic Tunnel No. 4 Results 5 by : P. Wegener
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:
Book Synopsis Nol Hypersonic Tunnel No. 4 Results Viii: Development and Calibration of Mass Flow Probes in Hypersonic Flow by : L. L. LICCINI
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:
Book Synopsis NOL Hypersonic Tunnel No. 4 Results IV: High Supply Temperature Measurement and Control by : Eva Winkler
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:
Book Synopsis NOL Hypersonic Tunnel No. 4 Results VII: Experimental Investiagtion of Turbulent Boundary Layers in Hypersonic Flow by : R. Kenneth Lobb
Download or read book NOL Hypersonic Tunnel No. 4 Results VII: Experimental Investiagtion of Turbulent Boundary Layers in Hypersonic Flow written by R. Kenneth Lobb and published by . This book was released on 1955 with total page 40 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis NOL Hypersonic Tunnel No. 4 Results III by : R. Kenneth Lobb
Download or read book NOL Hypersonic Tunnel No. 4 Results III written by R. Kenneth Lobb and published by . This book was released on 1952 with total page 14 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis NOL hypersonic tunnel no. 4 results II by : Peter P. Wegener
Download or read book NOL hypersonic tunnel no. 4 results II written by Peter P. Wegener and published by . This book was released on 1952 with total page 41 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis NOL Hypersonic Tunnel No. 4 Results V by : Wegener Peter P.
Download or read book NOL Hypersonic Tunnel No. 4 Results V written by Wegener Peter P. and published by . This book was released on 1953 with total page 42 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis 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 by :
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:
Book Synopsis NOL Hypersonic Tunnel No. 4 Results VI by : E. M. Winkler
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:
Book Synopsis NOL Hypersonic Tunnel No. 4 Results 2: Diffuser Investigation by :
Download or read book NOL Hypersonic Tunnel No. 4 Results 2: Diffuser Investigation written by and published by . This book was released on 1952 with total page 45 pages. Available in PDF, EPUB and Kindle. Book excerpt: Results of a diffuser investigation in the continuous 12 x 12 cm on Hypersonic Tunnel No. 4 are presented. A brief introduction describes previous supersonic diffuser work. The diffuser investigated and the experimental techniques are then discussed. The results show first that air condensation has little or no effect on diffuser performance. Data on diffuser throat areas and overall pressure ratios needed to start and maintain hypersonic flow are given for a Mach number range from 5.9 to 9.6. The effect of two different throat locations and different diffuser configurations on tunnel performance is investigated. A peaked throat diffuser with 3 deg wall divergence aft of the throat was selected for a more detailed study. The pressure recovered by this optimum diffuser in the range 5.9
Book Synopsis NOL Hyperballistics Tunnel No. 4 Results I: Air Liquefaction by : P. Wegener
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.
Book Synopsis Performance Capability of the NOL Hypersonic Tunnel by : Frank P. Baltakis
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).
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 1964 with total page 228 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Handbook of Supersonic Aerodynamics by : Johns Hopkins University. Applied Physics Laboratory
Download or read book Handbook of Supersonic Aerodynamics written by Johns Hopkins University. Applied Physics Laboratory and published by . This book was released on 1966 with total page 364 pages. Available in PDF, EPUB and Kindle. Book excerpt:
