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 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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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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Wind-tunnel Measurements and Comparison with Flight of the Boundary Layer and Heat Transfer on a Hollow Cylinder at Mach 3

Wind-tunnel Measurements and Comparison with Flight of the Boundary Layer and Heat Transfer on a Hollow Cylinder at Mach 3 PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 52

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Analysis of Heat-Transfer Measurements from Two AEDC Wind Tunnels on the Shuttle External Tank

Analysis of Heat-Transfer Measurements from Two AEDC Wind Tunnels on the Shuttle External Tank PDF Author: K. W. Nutt
Publisher:
ISBN:
Category :
Languages : en
Pages : 82

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Book Description
Previous aerodynamic heating tests were conducted in the AEDC/VKF Supersonic Wind Tunnel (A) to aid in defining the design thermal environment for the Space Shuttle external tank. The quality of these data has been under discussion because of the effects of low tunnel enthalpy and slow model-injection rates. Recently the AEDC/VKF Hypersonic Wind Tunnel (C) was modified to provide a Mach 4 capability that has significantly higher tunnel enthalpy with more rapid model-injection rates. Tests were conducted in Tunnel C at Mach 4 to obtain data on the external tank for comparison with Tunnel A results. Data were obtained on a 0.0175-scale model of the Space Shuttle Integrated Vehicle at Re/ft = 4 million with the tunnel stagnation temperature varying from 740 to 1440 R. Model attitude varied from an angle of attack of -5 to 5 deg and an angle of sideslip of -3 to 3 deg. One set of data was obtained in Tunnel C at Re/Ft = 69 million for comparison with flight data. This report presents data comparisons betwen the two tunnels for numerous regions on the external tank. Tunnel-to-flight data comparisons are presented for a small number of locations on the nose of the external tank. Keywords: Heat transfer; Mach number; Reynolds number; Aerodynamic heating; Wind tunnel tests; Aerothermodynamics; Enthalpy.

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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Design and Calibration of an Arc-heated, Hypersonic, Low-density Wind Tunnel

Design and Calibration of an Arc-heated, Hypersonic, Low-density Wind Tunnel PDF Author: Ruth N. Weitmann
Publisher:
ISBN:
Category : Chemistry, Physical and theoretical
Languages : en
Pages : 36

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A Review of High-speed, Convective, Heat-transfer Computation Methods

A Review of High-speed, Convective, Heat-transfer Computation Methods PDF Author: Michael E. Tauber
Publisher:
ISBN:
Category : Aerodynamic heating
Languages : en
Pages : 44

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Wind-tunnel Measurements and Comparison with Flight of the Boundary Layer and Heat Transfer on a Hollow Cylinder at Mach 3

Wind-tunnel Measurements and Comparison with Flight of the Boundary Layer and Heat Transfer on a Hollow Cylinder at Mach 3 PDF Author: Robert L. Stallings
Publisher:
ISBN:
Category : Aerothermodynamics
Languages : en
Pages : 52

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Wind Tunnel Designs and Their Diverse Engineering Applications

Wind Tunnel Designs and Their Diverse Engineering Applications PDF Author: Noor Ahmed
Publisher: BoD – Books on Demand
ISBN: 9535110470
Category : Science
Languages : en
Pages : 232

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Book Description
This book is intended to be a valuable addition to students, engineers, scientists, industrialists, consultants and others providing greater insight into wind tunnel designs and their enormous research potential. It is a compilation of works from world experts on subsonic and supersonic wind tunnel designs, applicable to a diverse range of disciplines. The book is organised in two sections. The first section comprises of three chapters on various aspects of stationary and portable subsonic wind tunnel designs, followed by one chapter on supersonic wind tunnel and the final chapter discusses a method to address unsteadiness effects of fan blade rotation. The second section contains four chapters regarding wind tunnel applications across a multitude of engineering fields including civil, mechanical, chemical and environmental engineering.