Laminar heat-transfer distributions on biconics at incidence in hypersonic-hypervelocity flows

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National Aeronautics and Space Administration, Scientific and Technical Information Branch, For sale by the National Technical Information Service] , Washington, D.C, [Springfield, Va
Heat -- Transmission, Aerodynamics, Hyper
StatementCharles G. Miller, III, John R. Micol, and Peter A. Gnoffo
SeriesNASA technical paper -- 2213
ContributionsMicol, John R, Gnoffo, Peter A, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch
The Physical Object
Paginationiii, 141 p. :
ID Numbers
Open LibraryOL17979738M

Laminar heat-transfer distributions on biconics at incidence in hypersonic-hypervelocity flows. Washington, D.C.: National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va.: For sale by the National Technical Information Service], (OCoLC) Material Type.

Charles G. Miller has written: 'Table and charts of equilibrium normal shock and shock-tube properties for pure argon with velocities to 18 km/sec' -. Aerodynamics, Hypersonic. See also what's at your library, or elsewhere.

Download Laminar heat-transfer distributions on biconics at incidence in hypersonic-hypervelocity flows FB2

Broader terms: Aerodynamics, Supersonic; Mach number; Sound pressure; Aerodynamics; Narrower. Answers is the place to go to get the answers you need and to ask the questions you want.

Two efficient computational procedures based on the boundary layer equations and approximate relations areassessedin prediction of the laminar hypersonic flowfield for both the perfect gas and equilibrium air around the axisymmetric blunt body configurations.

For the boundary layer procedure, the boundary layer equationsutilize the integral matrix solution algorithm for the Author: Ramin Kamali Moghadam, Seyed Amir Hosseini. Why does stryver continually criticize and belittle sydney carton for his social lapses From Tales of two Cities book 2 chapter Wiki.

What did Woolf. Laminar heating distributions were measured at hypersonic-hypervelocity flow conditions on a percent-scale model of an aeroassisted vehiclee proposed for missions to a number of planets.

Miller, C. G., Micol, J. R., and Gnoffo, P. () “Laminar Heat-Transfer Distributions on Biconics at Incidence in Hypersonic-Hypervelocity Flows,” NASA TP Google Scholar Miller, C. () “Experimental and Predicted Heating Distributions for Biconics at Incidence in Air at M” NASA TP Cited by: 1.

Available in the National Library of Australia collection. Author: Gnoffo, Peter A; Format: Book, Microform; 1 v. Aerodynamic heating rate distributions induced by trailing edge controls on hypersonic aircraft configurations at Mach 8 [microform] / prepared by Louis G.

Kaufman II and Charles B. Johnson National Aeronautics and Space Administration [Washington, DC. Conservation equations and physical models for hypersonic air flows in thermal and chemical equilibrium [microform] / Peter A.

Gnoffo, Roop N. Gupta, Judy L. Shinn National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; For sale by the National Technical Information Service.

The NASA LaRC expansion tube was recommissioned by GASL three years ago for the purpose of conducting hypersonic combustion experiments at Mach 17 total enthalpy in clean air in “Laminar heat transfer distributions on biconics at incidence in hypersonic-hypervelocity flows,” NASA TP Google Scholar.

Morgan, R., Stalker, R., Bakos Cited by: C.G. Miller, J.R. III, Micol, P.A. Gnoffo, Laminar heat-transfer distribution on biconics at incidence in hypersonic-hypervelocity flows, NASA TP, Google Scholar View AbstractCited by: 4.

Heat. See also what's at Wikipedia, your library, or elsewhere. Broader terms: Electromagnetic waves; Physics; Related terms: Cold; Combustion; Fire; Temperature.

a reconsideration of the hysteresis phenomenon in the regular ⇄ mach reflection transition in truly nonstationary flows k. takayama and go ben-dor d.l. book, j.p.

Description Laminar heat-transfer distributions on biconics at incidence in hypersonic-hypervelocity flows EPUB

boris, i.b. bernstein and m.a. fry text: pdf (mb) three-dimensional effects in shock detachment from a wedge. Heat-transfer distributions on biconics at incidence in hypersonic-hypervelocity He, N2, air, and CO2 flows. NASA Technical Reports Server (NTRS) laminar, separated flows was conducted at the Calspan-University at Buffalo Research Center (CUBRC) in the Large Energy National Shock (LENS) tunnel.

The experimental data serves as a focus for a. The decade of the s saw great advances in heat-transfer measurement techniques. Optical methods became popular, along with several new heat-flux gages that are still in wide use today, as evidenced by the commercial heat-flux-gage manufacturers.

In the last 10 to 20 years, a number of new techniques have been developed and applied, which. Int. Heat Mass Transfer. Vol. 29, No. 12, pp.Printed in Great Britain /86 $+ Pergamon Journals Ltd. Heat transfer review of literature by:   Snow distribution and heat flow in the taiga.

SciTech Connect. Sturm, M. The trees of the taiga intercept falling snow and cause it to become distributed in an uneven.

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Lunar ash flow with heat transfer. NASA Technical Reports Server (NTRS) Pai, S. I.; Hsieh, T.; O'Keefe, J. The most important heat-transfer process in the ash flow. An approximate heating technique9 for laminar and turbulent flows is incorporated in the procedure.

Predictions based on these heating equations have been shown to yield good agreement with experimental ground- and flight-test data and with CFD predictions at planetary and earth-entry conditions (e.g. Refs. 3 and ).