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Sunday, October 11, 2020 | History

3 edition of An analysis of combustion studies in shock expansion tunnels and reflected shock tunnels found in the catalog.

An analysis of combustion studies in shock expansion tunnels and reflected shock tunnels

An analysis of combustion studies in shock expansion tunnels and reflected shock tunnels

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  • 39 Currently reading

Published by National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, For sale by the National Technical Information Service] in [Washington, DC], [Springfield, Va .
Written in English

    Subjects:
  • Shock tubes.,
  • Combustion.

  • Edition Notes

    StatementCasimir J. Jachimowski.
    SeriesNASA technical paper -- 3224., NASA technical paper -- 3224.
    ContributionsUnited States. National Aeronautics and Space Administration. Scientific and Technical Information Program.
    The Physical Object
    FormatMicroform
    Pagination1 v.
    ID Numbers
    Open LibraryOL14684304M

    Martinez Schramm, Jan und Sunami, Tesuji und Itoh, Katsuhiro und Hannemann, Klaus () Experimental Investigation of Supersonic Combustion in the HIEST and HEG Free Piston Driven Shock Tunnels. 46th AIAA/ASME/SAE/ASEE Joint Propulsion Conference, Juli , Nashville, USA. ISBN Dieses Archiv kann nicht den gesamten Text zur Cited by: 3. Focused laser differential interferometry is used to quantify the free-stream density perturbations in the T5 reflected-shock tunnel. The investigation of reflected-shock tunnel disturbances is motivated by the study of hypervelocity boundary-layer instability and transition. Past work on hypersonic wind-tunnel noise is briefly reviewed. New results are reported for hypervelocity air Cited by:

    Studies of aerothermal loads generated in regions of shock/shock interaction in hypersonic flow (SuDoc NAS ) [Holden, Michael S.] on *FREE* shipping on qualifying offers. Studies of aerothermal loads generated in regions of shock/shock interaction in hypersonic flow (SuDoc NAS )Author: Michael S. Holden. They USE shock waves for chemical kinetics studies, for materials studies, and smashing kidney stones; they STUDY the phenomena associated with flows involving shock waves, such as supersonic flow, explosions, detonations, volcanic eruptions, and, in this symposium, even such with-it topics as impact of Shoemaker-Levy on Jupiter and blast waves.

    Shock Testing Paves the Way for Floating Tunnels Centre for Advanced Structural Analysis, or CASA, could pave the way for an entirely new type of . Studies of separated flow structure and oscillating separation shock waves in shock-wave/turbulent boundary-layer interaction regions induced by a blunt protuberance. A numerical study of shock-wave reflections in nonequilibrium chemically reacting flows. Thrbulent spots in boundary layers in a free-piston shock-tunnel flow.


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An analysis of combustion studies in shock expansion tunnels and reflected shock tunnels Download PDF EPUB FB2

Get this from a library. An analysis of combustion studies in shock expansion tunnels and reflected shock tunnels. [Casimir J Jachimowski; United States. National Aeronautics and Space Administration. Scientific and Technical Information Program.].

The Primary Reflected Shock. If the nozzle entry is assumed to be small compared with the diameter of the driving tube, the end of the tube may be regarded as effectively dosed.

The velocity u 5 behind the reflected shock is then zero, and, under these conditions, the pressure ratio Ps~ acrossFile Size: 2MB. Expansion and shock tunnels are aerodynamic testing facilities with a specific interest in high speeds and high temperature testing.

Shock tunnels use steady flow nozzle expansion whereas expansion tunnels use unsteady expansion with higher enthalpy, or thermal both cases the gases are compressed and heated until the gases are released, expanding rapidly down.

Reflected shock tunnels (RST) and shockexpansion tubes/tunnels (SET) are the major test facilities in gasdynamic laboratories that may satisfy the above request. View Show abstract. Abstract. Reflected shock tunnels have been used for a variety of experiments relating to scramjet combustion over the years.

This paper describes three sets of experiments which were performed on T3 and T4, the free piston driven reflected shock tunnel at the Australian National University, and at the University of Queensland, and explains the methodology by which they were : R.

Morgan. Some recent computational studies of the potential influence of injector design variables on performance will be reviewed as an example of the application of CFD to hypersonic combustion modeling.

Casimir J., “An analysis of combustion studies in shock expansion tunnels and reflected shock tunnels,” NASA TP, July. Google by: 5. Reservoir of and Pressure Studies in the a Reflected-Shock Hypersonic Tunnel By K.

LAPWORTH and J. TOWNSEND Reports and Memoranda No. * December, Summary. Temperatures and pressures have been measured in the shock-heated gas upstream of the nozzle of a reflected-shock hypersonic Size: 3MB.

The major features of the LENS reflected shock tunnels and the LENS X expansion tunnel are presented together with measurements and numerical simulations to calibrate and validate their.

This first book in the Tunnels series boasts an intriguing premise. There's just something about underground caverns and civilizations that's almost automatically appealing, and this is a particularly rich and nasty one, with cultish overtones and hints of an ancient history.3/5.

An analysis of combustion studies in shock expansion tunnels and reflected shock tunnels / (Washington, D.C.: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, ), by Casimir J.

Jachimowski and Langley Research Center (page images at HathiTrust). Advances in Shock Tube Techniques for Fundamental Studies of Combustion Kinetics Ronald K. Hanson, David F. Davidson Stanford University Stanford CA, USA 1 Introduction Shock tubes can provide well-defined temperatures and pressures for combustion kinetics investigations that cover broad regimes of engineering and scientific interest.

In the reflected tunnel, high pressure and high temperature reservoir gas is made by compressing test air by incident shock wave and reflected shock wave. The requirement of efficient injection method and flame holding has motivated the study of mixing [6], [7], as well as combustion [6], of transverse injection into supersonic by: in high-enthalpy reflected shock tunnels.

The details of the secondary diaphragm rupture will affecl both the strength of the reflected shock generated and the rate of expansion experienced by the test gas as it accelerates under the influence of the unsteady expansion. This Note adopts a diaphragm inertia rupture model 3 assuming that the di.

The Handbook of Shock Waves contains a comprehensive, structured coverage of research topics related to shock wave phenomena including shock waves in gases, liquids, solids, and space. Shock waves represent an extremely important physical phenomena which appears to be of special practical importance in three major fields: compressible flow (aerodynamics).

A laser ignition system suitable for a hypersonic scramjet engine is considered. Wall-modeled large eddy simulation (LES) is used to study a scramjet-like geometry with a single hAuthor: Nicholas Gibbons, Rolf Gehre, Stefan Brieschenk, Vincent Wheatley.

The last part of the book deals with many detailed case studies on structures of numerous materials like steel, composites, and concrete structures. Shock, Impact and Explosion is devoted to research and practising engineers, designers, technologists, mathematician and specialists in computer-aided by: Weber, R.J., Mackay, J.S.: An Analysis of ramjet engines using supersonic combustion.

Technical NoteNACA () An Analysis of Combustion Studies in Shock Expansion Tunnels and Reflected Shock : D. Oberg, R. Boyce, L. Brown, K. Itoh, T. Komuro. preliminary studies of hypersonic combustion. HYPERSONIC COI_BUSTION STUDIES "Hypersonic Combustion of Hydrogen in a Shock Tunnel" Although static pressure levels were limited to approx/imately 20 kPa, it was found that it was possible to produce hypersonic combustion in a duct of 25 n_u x 51 mm cross section, with a length of Size: 5MB.“ An Analysis of Combustion Studies in Shock Expansion Tunnels and Reflected Shock Tunnels,” NASA Langley Research Center Rept.

TP, Hampton, VA, July Google Scholar [31] Lu F. and Marren D., Advanced Hypersonic Test Facilities, Vol.Progress in Astronautics and Aeronautics, edited by Lu F. and Marren D., AIAA, Reston Cited by: Combustion, Explosion, and Shock Waves (Russian: Fizika Goreniya i Vzryva, Физика горения и взрыва) is the English-language translated version of the Russian peer-reviewed scientific journal, Fizika Goreniya i covers the combustion of gases and materials, detonation processes, dispersal and transformation of substances, and shock-wave line: Physical chemistry of combustion.

7) “Tunnel Engineering” (Date of Publication = 12 March, ) Tunnel is an underground passageway or a tube hollowed through soil or stone, completely enclosed except for openings for entrance and exit, commonly at each end.

Tunnels are used for mining, as passageways for trains and motor vehicles, for diverting rivers around dam sites, for housing underground installations .The book also contains recent progress in shock tube and shock tube tunnel technology, including free piston shock tunnels, diaphragmless shock tubes, various processes for improving shock tube performances and numerous diagnostic techniques used in millisecond facilities such as force, moment measurements and optical methods.Stationary hypersonic airflow behind the nozzle of a non-reflected shock tunnel represents an event of quite short duration within a long sequence of various flow phenomena.

This is a well-known fact which has been recognized since the beginning of shock tunnel studies ().