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Performance Capability Of The Nol Hypersonic Tunnel
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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 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 Wind-tunnel Study of Oscillating Flow-induced Surface Pressures on a Tension-cone Geometry Model by : Frank P. Baltakis
Download or read book Wind-tunnel Study of Oscillating Flow-induced Surface Pressures on a Tension-cone Geometry Model written by Frank P. Baltakis and published by . This book was released on 1974 with total page 62 pages. Available in PDF, EPUB and Kindle. Book excerpt: Oscillating flow about a spiked body in a supersonic stream has been investigated in a wind tunnel at Mach 5 at free-stream unit Reynolds numbers of 2,500,000 to 20,000,000 per foot using fast-response pressure transducers, accelerometers and schlieren movie cameras. A tension-cone-type model with replaceable nosetips of two different lengths and two different surface roughnesses was used.
Book Synopsis Experimental Investigation of a Fin-cone Interference Flow Field at Mach 5 by : Gillerlain, Jr. (Joseph D.)
Download or read book Experimental Investigation of a Fin-cone Interference Flow Field at Mach 5 written by Gillerlain, Jr. (Joseph D.) and published by . This book was released on 1976 with total page 86 pages. Available in PDF, EPUB and Kindle. Book excerpt: The general purpose of this investigation was to study the separated flow field associated with a fin-body juncture. Specific objectives included: (a) determining the severity and extent of aerodynamic heating, (b) providing flow visualization results to illustrate the flow structure, and (c) obtaining a data base of heat-transfer and surface-pressure measurements upon which to develop future analytical relations to predict peak interference heating levels. Tests were conducted at Mach 5 over a unit Reynolds number range of 4.5 to 26 million per foot. A fin-cone model was used. The data consist of surface- pressure distributions, heat-transfer measurements using the phase-change paint technique, and schlieren and oil-flow photographs. Results are presented for several fin-cone geometries to include fin sweep and fin-cone gap. Where possible, comparisons are made with fin-flat-plate data.
Book Synopsis Use of Phase-change Paints to Study Fin-body Interference Heating by : Gillerlain, Jr. (Joseph D.)
Download or read book Use of Phase-change Paints to Study Fin-body Interference Heating written by Gillerlain, Jr. (Joseph D.) and published by . This book was released on 1976 with total page 52 pages. Available in PDF, EPUB and Kindle. Book excerpt: In recent years the phase-change paint technique has evolved into an accepted diagnostic tool in high-speed wind-tunnel testing. This report documents use of the method at the Naval Surface Weapons Center, White Oak Laboratory, to study aerodynamic interference heating on fin-body configurations. Various aspects of both the underlying theory and the experimental method are enumerated based on experience and on information from other researchers. Analytic relationships are presented which indicate how uncertainties in the various input parameters affect the uncertainty in the heat-transfer coefficient. Advantages and disadvantages of the phase-change paint method are discussed.
Book Synopsis Advanced Hypersonic Test Facilities by : Frank K. Lu
Download or read book Advanced Hypersonic Test Facilities written by Frank K. Lu and published by AIAA. This book was released on 2002 with total page 694 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Influence of Roughness on Heat Transfer and Transition by : R. E. Phinney
Download or read book Influence of Roughness on Heat Transfer and Transition written by R. E. Phinney and published by . This book was released on 1973 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt: In order to assess the direct influence of surface roughtness upon heat transfer andits indirect effect through the shift in transition location, a series of wind tunnel tests were carried out. A fixed body shape (with one exception) with varying roughness was tested at a series of tunnel conditions and the heat transfer measured by the thin wall calorimenter method. The wind tunnel conditions and the heat transfer distribution around the models are presented in tabular form.
Book Synopsis Design and Performance of the University of Michigan 6.6-inch Hypersonic Wind Tunnel by : James L. Amick
Download or read book Design and Performance of the University of Michigan 6.6-inch Hypersonic Wind Tunnel written by James L. Amick and published by . This book was released on 1975 with total page 88 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis 48-inch Hypersonic Shock Tunnel by : Cornell Aeronautical Laboratory
Download or read book 48-inch Hypersonic Shock Tunnel written by Cornell Aeronautical Laboratory and published by . This book was released on 1962 with total page 46 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Proceedings of the International Instrumentation Symposium by :
Download or read book Proceedings of the International Instrumentation Symposium written by and published by . This book was released on 1980 with total page 864 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book NASA Technical Note written by and published by . This book was released on 1972 with total page 554 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis A Collection of Technical Papers by :
Download or read book A Collection of Technical Papers written by and published by . This book was released on 1970 with total page 888 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Scientific and Technical Aerospace Reports by :
Download or read book Scientific and Technical Aerospace Reports written by and published by . This book was released on 1994 with total page 584 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Laminar, Transitional, and Turbulent Heat Transfer Measurements on a Yawed Blunt Conical Nosetip by : George F. Widhopf
Download or read book Laminar, Transitional, and Turbulent Heat Transfer Measurements on a Yawed Blunt Conical Nosetip written by George F. Widhopf and published by . This book was released on 1972 with total page 100 pages. Available in PDF, EPUB and Kindle. Book excerpt: Laminar, transitional, and turbulent heat-transfer rates measured on a blunt (nose radius = 2.5 in.) 9-deg half-angle cone in a M freestream conditions = 5 air flow at various angles of attack are presented. Measurements were made at nominal freestream Reynolds numbers of 48.5, 19, 11, and 4.6 time 10 to the 6th power per foot at nominal angles of attack alpha = 0, 5, 10, 15, 20, and 27 degrees. The wall-to-stagnation temperature ratio varied between 0.20 and 0.29. Detailed circumferential and axial distributions of both the heat transfer rate and surface pressure were obtained over the entire model at each test condition and angle of attack. (Author).
Book Synopsis Technical Publications Announcements with Indexes by : United States. National Aeronautics and Space Administration
Download or read book Technical Publications Announcements with Indexes written by United States. National Aeronautics and Space Administration and published by . This book was released on 1962 with total page 1318 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Wind Tunnel Test Techniques by : Colin Britcher
Download or read book Wind Tunnel Test Techniques written by Colin Britcher and published by Academic Press. This book was released on 2023-10-20 with total page 672 pages. Available in PDF, EPUB and Kindle. Book excerpt: Wind Tunnel Test Techniques: Design and Use at Low and High Speeds with Statistical Engineering Applications provides an up-to-date treatment of the topic. Beginning with a brief history of wind tunnels and its types and uses, the book goes on to cover subsonic, supersonic and hypersonic wind tunnel design and construction, calibration, boundary corrections, flow quality assessment, pressure surveys, and dynamic testing. It also focuses on wind tunnel facilities, making it useful for both the designer and operator. Engineers and graduate students in aerospace, automotive and similar programs will find this book useful in their work with experimental aerodynamics, gas dynamics, facility design and performance. Deals with a broad range of flow speeds in wind tunnels, from low speed to high speed Provides a discussion of similarity laws as well as material on statistical analysis Includes coverage on facility-to-facility and facility-to-CFD correlation Presents advanced topics such as cryogenic wind tunnels, ground simulation in automotive testing, and propulsion testing
Book Synopsis NASA Technical Paper by : United States. National Aeronautics and Space Administration
Download or read book NASA Technical Paper written by United States. National Aeronautics and Space Administration and published by . This book was released on 1988 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
