3 edition of **Computations of axisymmetric flows in hypersonic shock tubes** found in the catalog.

Computations of axisymmetric flows in hypersonic shock tubes

- 36 Want to read
- 28 Currently reading

Published
**1995** by American Institute of Aeronautics and Astronautics, [National Aeronautics and Space Administration, National Technical Information Service, distributor in Washington, DC, Springfield, Va .

Written in English

- Computational fluid dynamics.,
- Axisymmetric flow.,
- Flow distribution.,
- Navier-Stokes equation.,
- Supersonic speed.

**Edition Notes**

Statement | Surendra P. Sharma and Gregory J. Wilson. |

Series | [NASA technical memorandum] -- 207282., NASA technical memorandum -- 207282. |

Contributions | Wilson, Gregory J., United States. National Aeronautics and Space Administration. |

The Physical Object | |
---|---|

Format | Microform |

Pagination | 1 v. |

ID Numbers | |

Open Library | OL15539928M |

(e-book CFD) - A Design Study of Single-Rotor Turbomachinery Cycles - 3-D Computational Fluid Dynamics For Gas And Gas-Particle Flows In A Cyclone With Different Inlet Section Specification For Seamless Cold-Drawn Low-Carbon Steel Heat-Exchanger And Condenser Tubes(1).pdf. Whitfield, D. L. and Lewis, C. H., "Analysis of Boundary Layers in Low Density Hypersonic Axisymmetric Nozzles, Including the Effects of Displacement, First-Order Transverse Curvature, Velocity Slip, and Temperature Jump," AIAA Paper No. , June Eric J. Ching, Yu Lv, Peter Gnoffo, Michael Barnhardt and Matthias Ihme, Shock capturing for discontinuous Galerkin methods with application to predicting heat transfer in hypersonic flows, Journal of Computational Physics, /, , (), ().Cited by: Introduction to hypersonic aerodynamics ~differences between hypersonic aerodyna mics and supersonic aerodynamics ~concept of thin shock layers and entropy layer s ~hypersonic flight paths ~hypersonic similarity parameters ~shock wave and exp ansion wave relations of inviscid hypersonic flows.

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Get this from a library. Computations of axisymmetric flows in hypersonic shock tubes. [Surendra Prasad Sharma; Gregory J Wilson; United States. National Aeronautics and.

What is axisymmetric. Unanswered Questions. Which was not a result of the baby boom that followed world war ii answers APEX. What are the examples of eleemosynary corporation. Modelling the complete operation of a free-piston shock tunnel for a low enthalpy condition Sharma, S.P., Wilson, G.J.: Computations of axisymmetric flows in hypersonic shock tubes.

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The challenges in understanding hypersonic flight are discussed and critical hypersonic aerothermodynamics issues are reviewed. The ability of current analytical methods, numerical methods, ground testing capabilities, Computations of axisymmetric flows in hypersonic shock tubes book flight testing approaches to predict hypersonic flow are evaluated.

The areas where aerothermodynamic shortcomings restrict our ability to Cited by: The relevant topic was referred to by Glass many years ago in his book entitled “Shock Waves and Man”, in which a series of photographs show the emergence of a inch-diameter bullet from a rifle at feet per second (M p =2).

An experimental study on axisymmetric supersonic flows around cylindrical projectiles has been presented by Matsumura et al.

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This proceedings book presents the results of the 31st International Symposium on Shock Waves (ISSW31), held in Nagoya, Japan in It covers among others blast waves, chemical reacting flows, chemical kinetics, detonation and combustion, flow visualization, and shock waves in.

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If the address matches an existing account you will receive an email with instructions to reset your password. Shock-induced three-dimensional separation of an axisymmetric hypersonic turbulent boundary layer.

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Similar computations are carried out for a specific trans-Alfvénic normal shock. An analytic asymptotic solution, valid for large times, is also obtained.

This result agrees with the computations carried out. The shock profile of the transverse quantities is one which grows linearly with time. Convertiplanes. See also what's at Wikipedia, your library, or elsewhere.

Broader terms: Airplanes; Helicopters; Vertically rising aircraft; Narrower term: Fairey. Filed under: Fluidized-bed combustion. Test and evaluation period ofpph atmospheric fluidized bed combustion boiler with 3, kw cogenerated electric power / ([Springfield, Ill.]: Illinois Dept. of Energy and Natural Resources, []), by Midwest Solvents Company of Illinois, Bibb and Associates, and Illinois.

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