NOL Hypersonic Tunnel No. 4 Results 2: Diffuser Investigation

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ISBN 13 :
Total Pages : 45 pages
Book Rating : 4.:/5 (227 download)

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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

NOL Hypersonic Tunnel No. 4

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ISBN 13 :
Total Pages : 84 pages
Book Rating : 4.3/5 (91 download)

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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).

U.S. Government Research Reports

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ISBN 13 :
Total Pages : 466 pages
Book Rating : 4.3/5 (243 download)

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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:

Effect of a Variable-geometry Diffuser on the Operating Characteristics of a Helium Tunnel Designed for a Mach Number in Excess of 20

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ISBN 13 :
Total Pages : 24 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis Effect of a Variable-geometry Diffuser on the Operating Characteristics of a Helium Tunnel Designed for a Mach Number in Excess of 20 by : Patrick J. Johnston

Download or read book Effect of a Variable-geometry Diffuser on the Operating Characteristics of a Helium Tunnel Designed for a Mach Number in Excess of 20 written by Patrick J. Johnston and published by . This book was released on 1960 with total page 24 pages. Available in PDF, EPUB and Kindle. Book excerpt:

NACA Research Memorandum

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ISBN 13 :
Total Pages : 82 pages
Book Rating : 4.F/5 ( download)

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Book Synopsis NACA Research Memorandum by :

Download or read book NACA Research Memorandum written by and published by . This book was released on 1957 with total page 82 pages. Available in PDF, EPUB and Kindle. Book excerpt:

NASA Technical Note

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ISBN 13 :
Total Pages : 424 pages
Book Rating : 4.:/5 (319 download)

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Book Synopsis NASA Technical Note by :

Download or read book NASA Technical Note written by and published by . This book was released on 1971 with total page 424 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Technical Note - National Advisory Committee for Aeronautics

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ISBN 13 :
Total Pages : 790 pages
Book Rating : 4.E/5 ( download)

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Book Synopsis Technical Note - National Advisory Committee for Aeronautics by : United States. National Advisory Committee for Aeronautics

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 1955 with total page 790 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Papers Presented at the Meeting of the Wind Tunnel and Model Testing Panel

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ISBN 13 :
Total Pages : 458 pages
Book Rating : 4.3/5 (243 download)

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Book Synopsis Papers Presented at the Meeting of the Wind Tunnel and Model Testing Panel by : North Atlantic Treaty Organization. Advisory Group for Aeronautical Research and Development

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:

Comparison Between Theoretical and Experimental Stresses in Circular Semimonocoque Cylinders with Rectangular Cutouts

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ISBN 13 :
Total Pages : 702 pages
Book Rating : 4.F/5 ( download)

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Book Synopsis Comparison Between Theoretical and Experimental Stresses in Circular Semimonocoque Cylinders with Rectangular Cutouts by : Harvey G. McComb

Download or read book Comparison Between Theoretical and Experimental Stresses in Circular Semimonocoque Cylinders with Rectangular Cutouts written by Harvey G. McComb and published by . This book was released on 1955 with total page 702 pages. Available in PDF, EPUB and Kindle. Book excerpt: Comparisons are made between a theory for calculating stresses about rectangular cutouts in circular cylinders of semimonocoque construction published in NACA TN 3200 and previously published NACA experimental data. The comparisons include stresses in the stringers and shear stresses in the center of the shear panels in the neighborhood of the cutout. The theory takes into account the bending flexibility of the rings in the structure, and this factor is found to be important in the calculation of stresses about cutouts. In general, when the ring flexibility is considered, good agreement is exhibited between the calculated and experimental results.

Starting Phenomena for Hypersonic Inlets with Thick Turbulent Boundary Layers at Mach 6

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ISBN 13 :
Total Pages : 68 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis Starting Phenomena for Hypersonic Inlets with Thick Turbulent Boundary Layers at Mach 6 by : Theodore J. Goldberg

Download or read book Starting Phenomena for Hypersonic Inlets with Thick Turbulent Boundary Layers at Mach 6 written by Theodore J. Goldberg and published by . This book was released on 1971 with total page 68 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Technical Information Pilot

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ISBN 13 :
Total Pages : 652 pages
Book Rating : 4.:/5 (319 download)

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Book Synopsis Technical Information Pilot by :

Download or read book Technical Information Pilot written by and published by . This book was released on 1952 with total page 652 pages. Available in PDF, EPUB and Kindle. Book excerpt:

AG [document]

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ISBN 13 :
Total Pages : 1120 pages
Book Rating : 4.3/5 (91 download)

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Book Synopsis AG [document] by : North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development

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:

WADC Technical Report

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ISBN 13 :
Total Pages : 1338 pages
Book Rating : 4.3/5 (91 download)

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Book Synopsis WADC Technical Report by : United States. Wright Air Development Division

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:

High Speed Problems of Aircraft and Experimental Methods

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Publisher : Princeton University Press
ISBN 13 : 140087503X
Total Pages : 1021 pages
Book Rating : 4.4/5 (8 download)

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Book Synopsis High Speed Problems of Aircraft and Experimental Methods by : Allen F. Donovan

Download or read book High Speed Problems of Aircraft and Experimental Methods written by Allen F. Donovan and published by Princeton University Press. This book was released on 2015-12-08 with total page 1021 pages. Available in PDF, EPUB and Kindle. Book excerpt: Volume VIII of the High Speed Aerodynamics and Jet Propulsion series. This volume includes: performance calculation at high speed; stability and control of high speed aircraft; aeroelasticity and flutter; model testing; transonic wind tunnels; supersonic tunnels; hypersonic experimental facilities; low density wind tunnels; shock tube; wind tunnel measurements; instrumented models in free flight; piloted aircraft testing; free flight range methods. Originally published in 1961. The Princeton Legacy Library uses the latest print-on-demand technology to again make available previously out-of-print books from the distinguished backlist of Princeton University Press. These editions preserve the original texts of these important books while presenting them in durable paperback and hardcover editions. The goal of the Princeton Legacy Library is to vastly increase access to the rich scholarly heritage found in the thousands of books published by Princeton University Press since its founding in 1905.

Papers

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ISBN 13 :
Total Pages : 674 pages
Book Rating : 4.:/5 (43 download)

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Book Synopsis Papers by : North Atlantic Treaty Organization. Advisory Group for Aeronautical Research and Development

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:

Subject Index to Unclassified ASTIA Documents

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ISBN 13 :
Total Pages : 922 pages
Book Rating : 4.3/5 (91 download)

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Book Synopsis Subject Index to Unclassified ASTIA Documents by : Defense Documentation Center (U.S.)

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:

Design and Operation of a Continuous-flow Hypersonic Wind Tunnel Using a Two-dimensional Nozzle

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ISBN 13 :
Total Pages : 304 pages
Book Rating : 4.3/5 (91 download)

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Book Synopsis Design and Operation of a Continuous-flow Hypersonic Wind Tunnel Using a Two-dimensional Nozzle by : Harris M. Schurmeier

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: