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  • Conference proceedings
  • © 1991

Hypersonic Flows for Reentry Problems

Volume II: Test Cases — Experiments and Computations Proceedings of a Workshop Held in Antibes, France, 22–25 January 1990

Editors:

  1. Jean-Antoine Désidéri

    1. Centre de Sophia Antipolis, INRIA, Valbonne Cedex, France

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  2. Roland Glowinski

    1. Department of Mathematics, University of Houston, Texas, Houston, USA

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  3. Jacques Périaux

    1. Aerodynamics Department, Dassault Aviation, Saint Cloud, France

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Table of contents (80 papers)

  1. Front Matter

    Pages I-XIII
    PDF

  2. Problems for Analysis

    1. Front Matter

      Pages 1-5
      PDF

    2. Problem 1: Flow over a Slender Cone

      • Jean-Antoine Désidéri, Roland Glowinski, Jacques Périaux
      Pages 6-7

    3. Problem 2 : Turbulent Base Flow

      • Jean-Antoine Désidéri, Roland Glowinski, Jacques Périaux
      Pages 8-9

    4. Problem 3: Flow over a 2D Ramp

      • Jean-Antoine Désidéri, Roland Glowinski, Jacques Périaux
      Pages 10-12

    5. Problem 4 : Flow over a 3-D Obstacle

      • Jean-Antoine Désidéri, Roland Glowinski, Jacques Périaux
      Pages 13-14

    6. Problem 5: Corner Flow

      • Jean-Antoine Désidéri, Roland Glowinski, Jacques Périaux
      Pages 15-16

    7. Problem 6: Double (Simple) Ellipsoid

      • Jean-Antoine Désidéri, Roland Glowinski, Jacques Périaux
      Pages 17-24

    8. Problem 7: Flow over a Delta Wing

      • Jean-Antoine Désidéri, Roland Glowinski, Jacques Périaux
      Pages 25-30

    9. Problem 8: Non-equilibrium Flow in an Arc Jet or a Shock Tube

      • Jean-Antoine Désidéri, Roland Glowinski, Jacques Périaux
      Pages 31-36

  3. Back Matter

    Pages 37-39
    PDF
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About this book

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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Keywords

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Editors and Affiliations

  • Centre de Sophia Antipolis, INRIA, Valbonne Cedex, France

    Jean-Antoine Désidéri

  • Department of Mathematics, University of Houston, Texas, Houston, USA

    Roland Glowinski

  • Aerodynamics Department, Dassault Aviation, Saint Cloud, France

    Jacques Périaux

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Bibliographic Information

  • Book Title: Hypersonic Flows for Reentry Problems

  • Book Subtitle: Volume II: Test Cases — Experiments and Computations Proceedings of a Workshop Held in Antibes, France, 22–25 January 1990

  • Editors: Jean-Antoine Désidéri, Roland Glowinski, Jacques Périaux

  • DOI: https://doi.org/10.1007/978-3-642-76527-8

  • Publisher: Springer Berlin, Heidelberg

  • eBook Packages: Springer Book Archive

  • Copyright Information: Springer-Verlag Berlin Heidelberg 1991

  • eBook ISBN: 978-3-642-76527-8Published: 06 December 2012

  • Edition Number: 1

  • Number of Pages: XIII, 1230

  • Number of Illustrations: 389 b/w illustrations, 8 illustrations in colour

  • Topics: Mathematical Methods in Physics, Numerical and Computational Physics, Simulation, Fluid- and Aerodynamics, Numerical Analysis

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Buy it now

eBook USD 74.99
Price excludes VAT (USA)
  • Available as PDF
  • Read on any device
  • Instant download
  • Own it forever

Tax calculation will be finalised at checkout

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