THERMODYNAMIC EFFECTS OF CAVITATION OF AN 80.6(DEGREE) HELICAL INDUCER OPERATED IN HYDROGEN

By Moore,Royce D. Nasa, Washington, D.C. 1970 . 12 , Bound With Nasa Tn D-5611-18

Place Hold on THERMODYNAMIC EFFECTS OF CAVITATION OF AN 80.6(DEGREE) HELICAL INDUCER OPERATED IN HYDROGEN

CHANGE IN INDUCER NET POSITIVE SUCTION HEAD REQUIREMENT WITH FLOW COEFFICIENT IN LOW TEMPERATURE HYDROGEN(27.9 [DIGREY] TO 36.6 [DIGREY] R)

By Meng,Phillip R. Nasa, Washington, D.C. 1986 . 25 , Bound With Nasa Tn D-4421-30

Place Hold on CHANGE IN INDUCER NET POSITIVE SUCTION HEAD REQUIREMENT WITH FLOW COEFFICIENT IN LOW TEMPERATURE HYDROGEN(27.9 [DIGREY] TO 36.6 [DIGREY] R)

INVESTIGATION OF TWO-PHASE HYDROGEN FLOW IN PUMP INLET LINE

By Urasek,Donald C, Meng,Phillip R. Nasa, Washington, D.C. 1969 . 11 , Bound With Nasa Tn D-5251-60

Place Hold on INVESTIGATION OF TWO-PHASE HYDROGEN FLOW IN PUMP INLET LINE

Effect of blade leading edge thickness on cavitation performance of 80.6 degree helical inducer in hydrogen [NASA TN D-5855]

By Moore, Royce D.. Washington, D.C. Nasa 1970 . 21p , Bound With Nasa Tn D-5851-5854,5856-5860

Place Hold on Effect of blade leading edge thickness on cavitation performance of 80.6 degree helical inducer in hydrogen [NASA TN D-5855]

NASA Technical Note [D-6350-6356, 6358-6363, 6365-6368]

Washington National Aeronautics and Space Administration (NASA) 1971 , NASA Technical Note [D-6350]: Critical speeds of a rotor in rigidly mounted, externally pressurized, air-lubricated bearings/ by Robert E. Cunningham and Edward J.Gunter | NASA Technical Note [D-6351]: Optimization of self-acting herringbone journal bearings for maximum radial load capacity/ by Bernard J. Hamrock and David P. Fleming | NASA Technical Note [D-6352]: Effect of exit temperature sampling density on measured combustor performance/ Robert E. Jones | NASA Technical Note [D-6353]: Friction and wear of poly(amide-imide), polymide, and pyrrone polymers at 260 degree C(500 degree F) in dry air / by William R. Jones, Jr. , William F. Hady, and Robert L Johnson | NASA Technical Note [D-6354]: Resonance Tube ignition of Hydrozen- Oxygen mixture/ by Bert R. Phillips and Albert J. Pavli | NASA Technical Note [D-6355]: Comparison of simplex and dual-orifici fuel nozzles with ambient and heated fuel in an annular turbojet combustor/ by Donald F. Schultz, Jerrold D. Wear, and Porter J. Perkins | NASA Technical Note [D-6356]: Molecular dynamics of polar gas rotational relaxation/ by Frank J. Zeleznik, John V. Dugan, and Raymond W. Palmer | NASA Technical Note [D-6358]: Radiation-Induced prepration of antimony from solutions of antimony (III) chaloride in organic liquids/ by Warren H. Philipp and Stanley J. Marsik | NASA Technical Note [D-6359]: Influence of aluminum on Friction and wear of iron-aluminum alloys dry and lubricated/ by Donald H. Buckley | NASA Technical Note [D-6360]: Combustor liner film cooling in the presence of high free-stream turbulence/ Albert J. Juhasz and Cecil J. Marek | NASA Technical Note [D-6361]: Comparison of noncavitation and cavitation performance for 78 degree , 80.6 degree, and 84 degree helical inducers operated in Hydrogen/ Royce D Moore and Phillip R. Meng | NASA Technical Note [D-6362]: Shorting path mode of degradation in copper sulfide - cadmium sulfide thin-film solar cells/ by Larry R. Scudder, Michael P. Godlewski, John M. Bozek, and Thomas M. Klucher | NASA Technical Note [D-6363]: Friction and wear of sintered tungsten, molybdenum, and cobalt- molybdenum impregnated with a fluoride eutectic/ Harold E. Sliney and Robert L. Fusaro | NASA Technical Note [D-6365]:Utilization of halo orbits in advanced lunar operations/ Robert W. Farquhar | NASA Technical Note [D-6366]: Effect of surface films on deformation of Zinc single-crystal surface during sliding/ Donald H. Buckley | NASA Technical Note [D-6367]: Effect of contact angle on rolling-element fatigue life with a fluorinated ether lubricant at a cryogenic temperature of 170 K (305 degree R)/ by Marshall W. Dietrich, Dennis P. Townsend, and Erwin V. Zaretsky | NASA Technical Note [D-6368]: Gas-jet impingement normal to a liquid surface/ Thomas L. Labus and John C. Aydelott

Place Hold on NASA Technical Note [D-6350-6356, 6358-6363, 6365-6368]

PKK Library Search for 'au:"Meng,Phillip R"'

THERMODYNAMIC EFFECTS OF CAVITATION OF AN 80.6(DEGREE) HELICAL INDUCER OPERATED IN HYDROGEN

CHANGE IN INDUCER NET POSITIVE SUCTION HEAD REQUIREMENT WITH FLOW COEFFICIENT IN LOW TEMPERATURE HYDROGEN(27.9 [DIGREY] TO 36.6 [DIGREY] R)

INVESTIGATION OF TWO-PHASE HYDROGEN FLOW IN PUMP INLET LINE

Effect of blade leading edge thickness on cavitation performance of 80.6 degree helical inducer in hydrogen [NASA TN D-5855]

NASA Technical Note [D-6350-6356, 6358-6363, 6365-6368]