Hypersonic Flows for Reentry Problems: Test Cases - Experiments and Computations Proceedings of a Workshop Held in Antibes, France, 22-25 January 1990

Author:   Jean-Antoine Desideri ,  Roland Glowinski ,  Jacques Periaux ,  J. Periaux (Dassault Aviation, St Cloud, France)
Publisher:   Springer-Verlag Berlin and Heidelberg GmbH & Co. KG
ISBN:  

9783540538592


Pages:   1243
Publication Date:   17 January 1992
Format:   Hardback
Availability:   Out of stock   Availability explained
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Hypersonic Flows for Reentry Problems: Test Cases - Experiments and Computations Proceedings of a Workshop Held in Antibes, France, 22-25 January 1990


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Overview

This entry describes the experimental work conducted in the Department of Aeronautics at Imperial College in connection with Test Problems 1 and 2 of the Workshop on Hypersonic Flows for Reentry Problems, Part I . These are defined as follows: Test Problem 1 Flow Over a Slender Cone Test Problem 2 Turbulent Base Flow The main requirement of this text is to present the experimental data for direct comparison with the predictions of CFD codes. We have therefore concentrated mainly on a factual statement of measuring techniques and results, together with an assessment of experimental accuracy. Future publications will be devoted to more extensive physical interpretations and discussions of the results. We have produced a large volume of data, some of which were categorised as MANDATORY and some as OPTIONAL for the purposes of CFD validation. However, only the MANDATORY data are presented here, although the other data are available and will be published separately later. 2. EXPERIMENTAL ARRANGEMENT 2. 1 The Test Facility The experiments were conducted in the Imperial College No. 2 Gun tunnel. This facility is a conventional intermittent blowdown tunnel with a contoured Mach 9 (nominal) axisymmetric nozzle fed by a free piston compression heater. The operating condition under which the data contained in this report were obtained is presented in Table 1. Test 2 T (oK) M b. Mlm Po (N/m ) Re/m T (oK) IX) IX) Case IX) w 1. 1 7 7 +0. 14 9. 16 6. 67x10 5. 5xl0 59.

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Author:   Jean-Antoine Desideri ,  Roland Glowinski ,  Jacques Periaux ,  J. Periaux (Dassault Aviation, St Cloud, France)
Publisher:   Springer-Verlag Berlin and Heidelberg GmbH & Co. KG
Imprint:   Springer-Verlag Berlin and Heidelberg GmbH & Co. K
Weight:   1.795kg
ISBN:  

9783540538592


ISBN 10:   3540538593
Pages:   1243
Publication Date:   17 January 1992
Audience:   College/higher education ,  Professional and scholarly ,  Postgraduate, Research & Scholarly ,  Professional & Vocational
Format:   Hardback
Publisher's Status:   Active
Availability:   Out of stock   Availability explained
The supplier is temporarily out of stock of this item. It will be ordered for you on backorder and shipped when it becomes available.

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