An Inexpensive Supersonic Wind Tunnel for Heat-transfer Measurements

An Inexpensive Supersonic Wind Tunnel for Heat-transfer Measurements PDF Author: Joseph Kaye
Publisher:
ISBN:
Category : Boundary layer
Languages : en
Pages : 23

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An Inexpensive Supersonic Wind Tunnel for Heat-transfer Measurements

An Inexpensive Supersonic Wind Tunnel for Heat-transfer Measurements PDF Author: Joseph Kaye
Publisher:
ISBN:
Category : Boundary layer
Languages : en
Pages : 23

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Book Description


AN INEXPENSIVE SUPERSONIC WIND TUNNEL FOR HEAT-TRANSFER MEASUREMENTS. PART 1. APPARATUS, DATA, AND RESULTS FOR A LAMINAR BOUNDARY LAYER BASED ON A SIMPLE ONE-DIMENSIONAL FLOW MODEL.

AN INEXPENSIVE SUPERSONIC WIND TUNNEL FOR HEAT-TRANSFER MEASUREMENTS. PART 1. APPARATUS, DATA, AND RESULTS FOR A LAMINAR BOUNDARY LAYER BASED ON A SIMPLE ONE-DIMENSIONAL FLOW MODEL. PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 42

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Design of a Small Supersonic Wind Tunnel for Heat Transfer Measurements at Mach Five

Design of a Small Supersonic Wind Tunnel for Heat Transfer Measurements at Mach Five PDF Author: Peter Ashurkoff
Publisher:
ISBN:
Category :
Languages : en
Pages : 170

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Design of an Inexpensive Supersonic Wind Tunnel with an Inlet Mach Number of Five for Heat Transfer Studies

Design of an Inexpensive Supersonic Wind Tunnel with an Inlet Mach Number of Five for Heat Transfer Studies PDF Author: John Russell Radbill
Publisher:
ISBN:
Category :
Languages : en
Pages : 88

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Hydraulic Research in the United States

Hydraulic Research in the United States PDF Author:
Publisher:
ISBN:
Category : Hydraulic engineering
Languages : en
Pages : 230

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Heat Transfer Measurements Using Narrow-band Liquid Crystals in a Supersonic Blowdown Wind Tunnel

Heat Transfer Measurements Using Narrow-band Liquid Crystals in a Supersonic Blowdown Wind Tunnel PDF Author: Hsieh-Hsiang Sam Chiu
Publisher:
ISBN:
Category : Heat
Languages : en
Pages :

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Report

Report PDF Author: United States. National Bureau of Standards
Publisher:
ISBN:
Category : Hydraulic engineering
Languages : en
Pages : 232

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Supersonic and Subsonic Wind Tunnel Heat-Transfer Measurements in the Base Cavity Region of the Shuttle Solid Rocket Booster During Simulated Reentry

Supersonic and Subsonic Wind Tunnel Heat-Transfer Measurements in the Base Cavity Region of the Shuttle Solid Rocket Booster During Simulated Reentry PDF Author: W. R. Hawkins
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ISBN:
Category :
Languages : en
Pages : 42

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Tests were conducted on the aft section of the Space Shuttle Solid Rocket Booster at Mach numbers 3.75 and 0.5 at selected angles of attack from 90-180 deg simulating reentry attitudes. The tests wre conducted in the AEDC Supersonic Wind Tunnel A to obtain heat-transfer coefficients in the base cavity region. (Author).

NBS Special Publication

NBS Special Publication PDF Author:
Publisher:
ISBN:
Category : Weights and measures
Languages : en
Pages : 226

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National Bureau of Standards Miscellaneous Publication

National Bureau of Standards Miscellaneous Publication PDF Author:
Publisher:
ISBN:
Category : Weights and measures
Languages : en
Pages : 220

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