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There are a total of 80698 record(s) matching your query.
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An analysis of laminar free-convection flow and heat transfer about a flat plate paralled to the direction of the generating body force
Author(s): Ostrach, Simon
Abstract: The free-convection flow and heat transfer (generated by a body force) about a flat plate parallel to the direction of the body force are formally analyzed and the type of flow is found to be dependent on the Grashof number ...
NASA Center: Glenn Research Center
Publication Year: 1953
Added to NTRS: 2009-01-14
Accession Number: 93R21437; Document ID: 19930092147; Report Number: NACA-TR-1111
Method of analysis for compressible flow through mixed-flow centrifugal impellers of arbitrary design
Author(s): Hamrick, Joseph T; Ginsburg, Ambrose; Osborn, Walter M
Abstract: A method is presented for analysis of the compressible flow between the hub and the shroud of mixed-flow impellers of arbitrary design. Axial symmetry was assumed, but the forces in the meridional (hub to shroud) plane, ...
NASA Center: Glenn Research Center
Publication Year: 1952
Added to NTRS: 2009-01-14
Accession Number: 93R21416; Document ID: 19930092126; Report Number: NACA-TR-1082
Analysis of plane-plastic stress problems with axial symmetry in strain-hardening range
Author(s): Wu, M H Lee
Abstract: A simple method is developed for solving plane-plastic-stress problems with axial symmetry in the strain-hardening range which is based on the deformation theory of plasticity employing the finite-strain concept. The ...
NASA Center: Glenn Research Center
Publication Year: 1951
Added to NTRS: 2009-01-14
Accession Number: 93R21366; Document ID: 19930092076; Report Number: NACA-TR-1021
Cloud-droplet ingestion in engine inlets with inlet velocity ratios of 1.0 and 0.7
Author(s): Brun, R. J.
Abstract: No Abstract Available
NASA Center: Glenn Research Center
Publication Year: 1957
Added to NTRS: 2009-01-14
Accession Number: 81N73120; Document ID: 19810068698; Report Number: NACA-TR-1317
Compressible laminar boundary layer over a yawed infinite cylinder with heat transfer and arbitrary Prandtl number
Author(s): Reshotko, Eli; Beckwith, Ivan E
Abstract: The equations are presented for the development of the compressible laminar boundary layer over a yawed infinite cylinder. For compressible flow with a pressure gradient the chordwise and spanwise flows are not independent. ...
NASA Center: Glenn Research Center
Publication Year: 1958
Added to NTRS: 2009-01-14
Accession Number: 93R21651; Document ID: 19930092361; Report Number: NACA-TR-1379
Calculations of laminar heat transfer around cylinders of arbitrary cross section and transpiration-cooled walls with application to turbine blade cooling
Author(s): Eckert, E R G; Livingood, J N B
Abstract: An approximate method for the development of flow and thermal boundary layers in the laminar region on cylinders with arbitrary cross section and transpiration-cooled walls is obtained by the use of Karman's integrated ...
NASA Center: Glenn Research Center
Publication Year: 1955
Added to NTRS: 2009-01-14
Accession Number: 93R21520; Document ID: 19930092230; Report Number: NACA-TR-1220
Temperature distribution in internally heated walls of heat exchangers composed of nonnuclear flow passages
Author(s): Eckert, E R G; Low, George M
Abstract: In the walls of heat exchangers composed of noncircular passages, the temperature varies in the circumferential direction because of local variations of the heat-transfer coefficients. A prediction of the magnitude of this ...
NASA Center: Glenn Research Center
Publication Year: 1951
Added to NTRS: 2009-01-14
Accession Number: 93R21367; Document ID: 19930092077; Report Number: NACA-TR-1022
Review of experimental investigations of liquid-metal heat transfer
Author(s): Lubarsky, Bernard; Kaufman, Samuel J
Abstract: Experimental data of various investigators of liquid-metal heat-transfer characteristics were reevaluated using as consistent assumptions and methods as possible and then compared with each other and with theoretical ...
NASA Center: Glenn Research Center
Publication Year: 1956
Added to NTRS: 2009-01-14
Accession Number: 93R20291; Document ID: 19930091001; Report Number: NACA-TR-1270
Theoretical combustion performance of several high-energy fuels for ramjet engines
Author(s): Tower, Leonard K; Breitwieser, Roland; Gammon, Benson E
Abstract: An analytical evaluation of the air and fuel specific-impulse characteristics of magnesium, magnesium octene-1 slurries, aluminum, aluminum octene-1 slurries, boron, boron octene-1 slurries, carbon, hydrogen, ...
NASA Center: Glenn Research Center
Publication Year: 1958
Added to NTRS: 2009-01-14
Accession Number: 93R20307; Document ID: 19930091017; Report Number: NACA-TR-1362
Axisymmetric supersonic flow in rotating impellers
Author(s): Goldstein, Arthur W
Abstract: General equations are developed for isentropic, frictionless, axisymmetric flow in rotating impellers with blade thickness taken into account and with blade forces eliminated in favor of the blade-surface function. It is ...
NASA Center: Glenn Research Center
Publication Year: 1952
Added to NTRS: 2009-01-14
Accession Number: 93R21417; Document ID: 19930092127; Report Number: NACA-TR-1083
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