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Monday, August 3, 2020 | History

2 edition of Development of the spark-heated, hypervelocity, blowdown tunnel-Hotshot found in the catalog.

Development of the spark-heated, hypervelocity, blowdown tunnel-Hotshot

R. W. Perry

Development of the spark-heated, hypervelocity, blowdown tunnel-Hotshot

by R. W. Perry

  • 116 Want to read
  • 31 Currently reading

Published by AF-AEDC in Tullahoma, Tenn .
Written in English

    Subjects:
  • Hypersonic wind tunnels.

  • Edition Notes

    Statementby R.W. Perry and W.N. MacDermott.
    SeriesAEDC-TR -- 58-6, ASTIA document -- no. AD-157138, ASTIA documents -- no. AD-157138.
    ContributionsMacDermott, W. N., Arnold Engineering Development Center., Defense Documentation Center (U.S.)
    Classifications
    LC ClassificationsTL567.W5 P47 1958
    The Physical Object
    Pagination103 leaves :
    Number of Pages103
    ID Numbers
    Open LibraryOL21694072M

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    Be sure that the blowdown mechanism is working properly. Monitor the control valve to ensure valve position has not changed significantly for a given operating condition. If the nozzle assembly were to fail completely, the flow coefficient (Cv) would be much higher than it would were the spray nozzles present. Thus the control valve would. Pendant SH - Tubes suspended vertically, usually for radiant SH's, located at the top of the furnace Horizontal SH - Tubes run horizontal, normally in a duct, Convection SH's are often horizontal type Integral - Are a part of the boiler setting and an integral part of a boiler or steam generator Separately Fired - Located in a dedicated furnace and independent of steam generator operating.


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Development of the spark-heated, hypervelocity, blowdown tunnel-Hotshot by R. W. Perry Download PDF EPUB FB2

DEVELOPMENT OF THE SPARK-HEATED, HYPERVELOCITY, BLOWDOWN TUNNEL-HOTSHOT R. Perry and W.N. MacDermott* 1. INTRODUCTION When the design of the present Gas Dynamics Facility (GDF) at the Arnold Engineering Development Center (AEDC) was initiated init was already realized that a con- ventional hypersonic tunnel would not reach Development of the spark-heated.

Test facilities of these types have been in development and operation for several years at the Missile and Space Vehicle Department of the General Electric Company.

To illustrate their usefulness, examples of experimental data obtained in the 6 Inch Shock Tunnel and in several arc heated facilities, including a KW (test gas power) unit Cited by: 4.

a 1-foot hypervelocity shock tunnel in which high-enthalpy, realgas air flows can be generated with flow times of about milliseconds by cunningham, b.

e.; kraus, s. Introduction The Hypervelocity Wind Tunnel No. 9 located at White Oak, Maryland, site of the Arnold Engineering Development Center (AEDC, formerly the Naval Surface Warfare Center [NSWC]) has long been recognized as a unique world-class, ground-test facility.

New hypervelocity capabilities for radiative heat transfer measurements have recently been demonstrated in the HyPulse Shock Tunnel. Until recently, the NASA Blowdown tunnel-Hotshot book facility at ATK GASL in. American Institute of Aeronautics and Astronautics Sunrise Valley Drive, Suite Reston, VA blowdown wind tunnel, thermal matrix, supersonic testing, isentropic flow, thermo-compensation.

Introduction. Blowdown wind tunnels [1, 2] use the energy of air stored in highpressure tanks. - During a wind tunnel. run, this air is let to flow through the settling chamber, the nozzle and the test section and then discharged into the at.

Axon's high-performance heat shrink tunnels are designed and built to meet the most challenging shrink applications. They are recognized in the industry for their flexibility and they are capable of shrinking multiple film substrates onto a wide range of container types, shapes and sizes.

But what exactly is HyperConvergence and why is it the lingo today. Instead of blindly plunging on the passage of adopting HyperConverged Infrastructure to meet the IT requirements and demands of your business, you need to know exactly what.

Acknowledgements. This work was supported by the National Natural Science Foundation of China (Grants,and ). Intermittent blow down and in draft tunnels are normally used for Mach numbers from to and the intermittent pressure -vacuum tunnels are normally used for higher Mach numbers.

uous Wind Tunnel Continuous wind tunnels are capable of operating for longer periods. The testing conditions can be. Shrink Tunnels. Industrial heat shrink tunnels use heat to shrink film around packages.

Shrink tunnel standard sizes range from 15” wide by 6” high up to 22” wide by 8” high, with varying lengths and extended heights. Hypervelocity Impact Test Results for a Metallic Thermal Protection System Katherine L.

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