4 edition of **Hypersonic flows for reentry problems.** found in the catalog.

- 203 Want to read
- 12 Currently reading

Published
**1991**
by Springer-Verlag in Berlin, New York
.

Written in English

- Space vehicles -- Atmospheric entry -- Congresses.,
- Aerodynamics, Hypersonic -- Congresses.,
- Space vehicles -- Atmospheric entry -- Problems, exercises, etc.,
- Aerodynamics, Hypersonic -- Problems, exercises, etc.

**Edition Notes**

Includes bibliographical references and index.

Contributions | Désidéri, J.-A. 1951- |

Classifications | |
---|---|

LC Classifications | TL1060 .H96 1991 |

The Physical Object | |

Pagination | v. <1, 3 > : |

ID Numbers | |

Open Library | OL1552833M |

ISBN 10 | 3540544283, 0387544283, 3540561897, 0387561897 |

LC Control Number | 91032792 |

Simulation of Radiation from Electronic Transitions in Hypersonic Atmospheric Reentry Flow. A capability for higher accuracy heat transfer modeling in CFD for hypersonic re-entry flows, via inclusion of thermal radiation, is sought. With temperatures reaching tensAuthor: Curtis Scholz. If there's one word that keeps military planners from sleeping at night, it's "hypersonic." The ability to fly at more than five times the speed of sound holds the promise of getting to the.

Challenges of Hypersonic Flight. by: Athena Roberts. Written: April Thankyou for inviting me over to speak with you all about Hypersonic Flight. In flight school, you might have briefly gone over this as a curiosity, so I will define hypersonic flight. We rather arbitrarily . at hypersonic flows. Sreekanth [11] have used secondary spike on a blunt head to reduce the drag coefficient. These results helped in selecting the geometrical parameters for the analysis of drag reduction on re-entry vehicles. An l/d ratio File Size: KB.

Verification of Engineering Methods of Aerodynamics for Reentry Vehicles by DSMC p. Numerical Modelling and Simulation of Chemically Reacting Reentry Flows p. Simulation of Hypersonic Flows Using Detailed Reaction and Transport Models p. Modelling of Chemical and Physical Effects with Respect to Flows Around Reentry Bodies p. File Size: 5KB. For hypersonic aircraft, three principle missions have been identified with each mission having its own unique vehicle requirements. Re-entry from Orbit. The earliest studied and most often encountered hypersonic flows involve the re-entry of a spacecraft from orbit around the earth. NASA's Mercury, Gemini, and Apollo spacecraft experienced.

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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.

This entry describes the experimental work conducted in the Department Hypersonic flows for reentry problems. book Aeronautics at Imperial College in connection with Test Problems 1 and 2 of the "Workshop on Hypersonic Flows for Reentry Problems, Part I". Problems and exercises Congresses Problems, exercises, etc: Additional Physical Format: Online version: Hypersonic flows for reentry problems.

Berlin ; New York: Springer-Verlag, © (OCoLC) Material Type: Conference publication: Document Type: Book: All Authors / Contributors: J -A Désidéri.

One of the most challenging problems of modern engineering is undoubtedly the prediction of hypersonic flows around space vehicles in reentry conditions. Indeed, the difficulties are numerous: first of all, these flows are very difficult to model, since very complex physical and chemical phenomena take place during the reentry phase; secondly Format: Paperback.

On the basis of this belief, the International Workshop on Hypersonic Flows for Reentry Problems, Part II, took place in Antibes, France, from 15 to 19 April This workshop, whose proceedings form this volume, was a clear continua tion of the Euro-American short courses on hypersonics held in Paris inColorado Springs inand Price: $ One of the most challenging problems of modern engineering is undoubtedly the prediction of hypersonic flows around space vehicles in reentry conditions.

Indeed, the difficulties are numerous: first of all, these flows are very difficult to model, since very complex physical and chemical phenomena. INRIA and GAMNI/SMAI have organized a Workshop open to the international scientific community on hypersonic flows for reentry problems which was held in Palais des Congres d'Antibes in January.

To download Hypersonic Flows for Reentry Problems: Volume I: Survey Lectures and Test Cases Analysis Proceedings of Workshop Held in Antibes, France, 22 25 January PDF, remember to follow the link beneath and save the ebook or have access to. Free 2-day shipping.

Buy Hypersonic Flows for Reentry Problems: Volume I: Survey Lectures and Test Cases Analysis Proceedings of Workshop Held in Antibes, France, January (Paperback) at Price: $ Hypersonic flows, however, require other similarity parameters.

First, the analytic equations for the oblique shock angle become nearly independent of Mach number at high (~>10) Mach numbers. Second, the formation of strong shocks around aerodynamic bodies means that the freestream Reynolds number is less useful as an estimate of the behavior.

Introduction to Hypersonic Flows. Hypersonic Flows for Reentry Problems. Book. Jun ; who made it possible for me to write and edit this book in the very quiet atmosphere of our home.

Hypersonic Flows for Reentry Problems Jean-Antoine Desideri,Roland Glowinski,Jacques Periaux — Science Volume II: Test Cases — Experiments and Computations Proceedings of a Workshop Held in Antibes, France, 22–25 January Get this from a library.

Hypersonic Flows for Reentry Problems: Volume II: Test Cases - Experiments and Computations Proceedings of a Workshop Held in Antibes, France, January [Jean-Antoine Désidéri; Roland Glowinski; Jacques Périaux] -- The physical modelling and the numerical simulation of the critical reentry phase of hypersonic space vehicles are important areas of.

W.H. Mason Hypersonic Aerodynamics 7/31/16 Figure Sketch defining the hypersonic directional stability problem Now, for a high-speed flow, we will assume that the vertical tail is a two-dimensional surface with a constant pressure on each side, so that.

We will consider two cases, one supersonic, the other Size: 1MB. Hypersonic flows for reentry problems Remi Abgrall, Jean-Antoine Desideri, Michel Mallet, Jacques Periaux, Pierre Perrier, Bruno Stoufflet To cite this version: Remi Abgrall, Jean-Antoine Desideri, Michel Mallet, Jacques Periaux, Pierre Perrier, et al.

Hyper-sonic flows for reentry problems. [Research Report] RR, INRIA. inria. Re-Entry Trajectories and Problems of Hypersonic Flow RUDOLF HERMANN University of Minnesota, Minneapolis, Minnesota * SYMBOLS a A Ac cm Cp C CD CL Coo D Di2 e e~ g G G* h ÄD Ae k km' kft Kn kw ZD L Le m Ms sound velocity cross section area cross section area centimeter specific heat at constant pressure a constant related to dissociation drag coeflScient lift coefficient factor in Author: Rudolf Hermann.

The mathematical and numerical formulation employed in the development of a new multi-dimensional Computational Fluid Dynamics (CFD) code for the simulation of weakly ionized hypersonic flows in thermo-chemical non-equilibrium over reentry configurations is presented.

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”.Cited by: 1.

The reentry trajectory optimization for hypersonic vehicle (HV) is a current problem of great interest. Some complex constraints, such as waypoints for reconnaissance and no-fly zones for threat avoidance, are inevitably involved in a global strike by: Hypersonic Flow Theory presents the fundamentals of fluid mechanics, focusing on the hypersonic flow theory and approaches in theoretical aerodynamics.

This book discusses the assumptions underlying hypersonic flow theory, unified supersonic-hypersonic similitude, two-dimensional and axisymmetric bodies, and circular Edition: 1.

T1 - Advanced radiation calculations of hypersonic reentry flows using efficient databasing schemes. AU - Sohn, I.

AU - Bansal, A. AU - Levin, D. A. AU - Modest, M. F. PY - /7/1. Y1 - /7/1. N2 - Efficient schemes for databasing emission and absorption coefficients are developed to model radiation from hypersonic nonequilibrium by: Facing the Heat Barrier: A History of Hypersonics.

T. A. Heppenheimer. Facing the Heat Barrier: A History of Hypersonics. T. A. Heppenheimer. Hypersonics is the study of flight at speeds where. aerodynamic heating dominates the physics of the problem.

Typically this is Mach 5 and higher. Hypersonics is an engineering science with close.NUMERICAL SIMULATION OF WEAKLY IONIZED HYPERSONIC FLOW OVER REENTRY CAPSULES by Leonardo C. Scalabrin A dissertation submitted in partial fulﬁllment of the requirements for the degree of Doctor of Philosophy (Aerospace Engineering) in The University of Michigan Doctoral Committee: Professor Iain D.

Boyd, Chairperson Professor Bram van LeerCited by: