The mechanism and application of effusion cooling

P Grootenhuis - The Aeronautical Journal, 1959 - cambridge.org
Effusion cooling consists in forcing a gas under pressure through a porous material thereby
absorbing heat from the material and forming a heat insulating layer on the exposed surface …

Experimental study of cooling by injection of a fluid through a porous material

P Duwez, HL Wheeler Jr - Journal of the Aeronautical Sciences, 1948 - arc.aiaa.org
SUMMARY A method of coping with the high rates of heat transfer encountered in the field of
jet-propulsion consists of making the parts to be cooled of a porous material and forcing the …

Heat transfer through sweat cooled porous tubes

HL Wheeler Jr, P Duwez - Journal of Jet Propulsion, 1955 - arc.aiaa.org
Introduction r^ HE results of experimental and theoretical studies of gaseous sweat cooling
described previously (1, 2) 3 have 3 Numbers in parentheses indicate References at end of …

Transpiration cooling in porous metal walls

E Mayer, JG Bartas - Journal of Jet Propulsion, 1954 - arc.aiaa.org
THE differential equations governing internal heat transfer and temperature distributions
within a porous medium under transpiration cooling have been formulated in (1) and (3). In …

Porous heat exchangers-classification, construction, application

VA Maiorov, LL Vasil'Ev, VM Polyaev - Journal of engineering physics, 1984 - Springer
Porous Coolin $ Elements. The method of transpirational cooling of structures on which
external convective or radiant heat flows of high density act (see Fig. i) has a number of …

[PDF][PDF] Transpiration Cooling-Its Theory and Application

JB Kelley, MR Lecuyer - 1966 - ntrs.nasa.gov
Transpiration cooling is one of the more promising solutions to the material's problem
imposed on high enemy liquid, solid and nuclear rocket engines, atmospheric reentry …

An approximate theory of porous, sweat, or film cooling with reactive fluids

L Crocco - Journal of the American Rocket Society, 1952 - arc.aiaa.org
THE conventional regenerative cooling of rocket motors is subject to severe limitations in
two cases:(a) When high energy propellants or high working pressures are used, since the …

The transpiration-cooled gas turbine

FJ Bayley, AB Turner - 1970 - asmedigitalcollection.asme.org
This paper describes a program of experimental and analytical research designed to
evaluate the aerodynamic and thermodynamic performance of transpiration-cooled porous …

[引用][C] Enhancement of cooling effectiveness by porous materials in coolant passage

JCY Koh, RL Stevens - 1975 - asmedigitalcollection.asme.org
In reference [l], 2 it was shown analytically that the cooling effectiveness of a regenerative
cooling scheme can be increased significantly by packing the coolant passage with porous …

[PDF][PDF] Exploratory tests of transpiration cooling on a porous 8 degree cone at M= 2.05 using nitrogen gas, helium gas, and water as the coolants

LT Chauvin, HS Carter - 1955 - ntrs.nasa.gov
The effectiveness of transpiration cooling on an 80 total-angle conical bo~ having a porous
skin is presented for various coolant mass flow rates of nitrogen gas, helium gas, and …