An isentropic compression-heated Ludweig tube transient wind tunnel-Reference-Cited by-同舟云学术

An isentropic compression-heated Ludweig tube transient wind tunnel

Published:1991-05 Issue:3 Volume:4 Page:317-332
ISSN:0894-1777
Container-title:Experimental Thermal and Fluid Science
language:en
Short-container-title:Experimental Thermal and Fluid Science

Author:

Magari Patrick J.,LaGraff John E.

Publisher

Elsevier BV

Subject

Fluid Flow and Transfer Processes,Mechanical Engineering,Aerospace Engineering,Nuclear Energy and Engineering,General Chemical Engineering

Reference15 articles.

1. A Ludweig Tube with Light Piston Isentropic Compression Heating;Oldfield;Aeronautical Research Council Reports and Memoranda No. 34255, HYP935,1973

2. Studies on Bodies of Revolution at High Mach Numbers;Grimshaw;Oxford Univ. Engineering Lab Report, QUEL 1182/77,1977

3. Free Flight Drag and Lift Coefficient and Heat Transfer Rates to a 7° Half Angle Blunted Cone;Robson;Oxford Univ. Engineering Lab Report, QUEL 1668/87,1987

4. Unsteady Heat Transfer in a Transient Facility;LaGraff;Annual progress report on NASA grant NAG 3-621,1986

5. A Long Stroke Isentropic Free Piston Hypersonic Wind Tunnel;East;Aeronautical Research Council Reports and Memoranda No. 3844,1978

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