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Propulsion system elements

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• Fluid mechanics; -- Propulsion system elements

• Theoretical analysis of effects of ablation on heat transfer to an arbitrary axisymmetric body (National Aeronautics and Space Administration :, 1961), by Robert T. Swann, Jerry C. South, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• The effect of thrust minus base drag of exchanging base area for nozzle expansion in supersonic nozzles at transonic mach numbers (National Aeronautics and Space Administration :, 1961), by Travis H. Slocumb, Earl H. Andrews, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Internal-performance evaluation of a two-position divergent shroud ejectro (National Aeronautics and Space Administration :, 1961), by James R. Mihaloew, Andrew J. Stofan, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Internal-performance evaluation of two fixed-divergent-shroud ejectors (National Aeronautics and Space Administration :, 1961), by James R. Mihaloew and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Effect of multiple-nozzle geometry on jet noise generation. (National Aeronautics and Space Administration :, 1961), by Vern G. Rollin and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Performance of a low-thrust storable propellant rocket at very low chamber pressure (National Aeronautics and Space Administration :, 1961), by John P. Wanhainen, Phil S. Ross, Richard L. DeWitt, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Ignition of hydrogen-oxygen rocket combustor with chlorine trifluoride and triethylaluminum (National Aeronautics and Space Administration :, 1961), by John W. Gregory, David M. Straight, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Large-scale wind-tunnel tests of exhaust ingestion due to thrust reversal on a four-engine jet transport during ground roll (National Aeronautics and Space Administration :, 1961), by William H. Tolhurst, Kiyoshi Aoyagi, David H. Hickey, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Charts for air flow properties in equilibrium and frozen flows in hypervelocity nozzles (National Aeronautics and Space Administration :, 1961), by Kenneth K. Yoshikawa, Elliott D. Katzen, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• An experimental investigation of the flow in an axisymmetric internal-compression inlet for M=2.75 (National Aeronautics and Space Administration :, 1961), by Earl C. Watson, William P. Peterson, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Ignition of a hydrogen-oxygen rocket engine by addition of fluorine to the oxidant (National Aeronautics and Space Administration :, 1962), by R. James Rollbuhler, David M. Straight, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Optical torquemeter for high rotational speeds / Alois Kresk Jr. and Marvin Tiefermann. (National Aeronautics and Space Administration :, 1962), by Alois Kresk, Marvin W. Tiefermann, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Performance evaluation of fixed- and variable-area rocket exhaust diffusers using single and clustered nozzles with and without gimbaling (National Aeronautics and Space Administration :, 1962), by Bruce E. Church, Richard J. Quentmeyer, William L. Jones, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Effects of simulated retrorockets on the aerodynamic characteristics of a body of revolution at Mach numbers from 0.25 to 1.90 (National Aeronautics and Space Administration :, 1962), by Victor L. Peterson, Robert L. McKenzie, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• A Use of conformal mapping to determine the apparent additional mass of scalloped and/or clustered cylinder configurations with experimental evaluations of results / Charles E. Watkins, Donald L. Lansing and Frederick W. Gibosn. (National Aeronautics and Space Administration :, 1962), by Charles E. Watkins, Frederick W. Gibson, Donald L. Lansing, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Analysis of magnetic triodes for direct-energy conversion having flat-plate cathodes and anodes at an arbitrary angle (National Aeronautics and Space Administration :, 1960), by James E. Hatch and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Liquid-hydrogen-flowmeter calibration facility; preliminary calibrations on some head-type and turbine-type flowmeters (National Aeronautics and Space Administration :, 1961), by Herbert L. Minkin, Howard F. Hobart, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• An experimental determination of the dynamic response of a long hydraulic line (National Aeronautics and Space Administration :, 1960), by John D. Regetz and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Effect of shield positioni and absorptivity on temperature distribution of a body shielded from solar radiation in space (National Aeronautics and Space Administration :, 1961), by Lester D. Nichols and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Experimental method of producing porous tungsten for ion rocket engines (National Aeronautics and Space Administration :, 1961), by Neal T. Saunders and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Effect of nozzle convergence length on performance of a heptane-oxygen combustor (National Aeronautics and Space Administration :, 1960), by Marshall C. Burrows and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Experimental damping of liquid oscillations in a spherical tank by positive-expulsion bags and diaphragms (National Aeronautics and Space Administration :, 1962), by Andrew J. Stofan, Albert J. Pavli, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Boiling heat transfer to liquid hydrogen and nitrogen in forced flow (National Aeronautics and Space Administration :, 1962), by James P. Lewis, John F. Kline, Jack H. Goodykoontz, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Design and performance of a liquid-hydrogen, liquid-oxygen gas generator for driving a 1000-horsepower turbine (National Aeronautics and Space Administration :, 1962), by Nick J. Sekas, Loren W. Acker, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Performance of several cast nickel-base alloys as turbojet-engine bucket materials at 1650° F (National Aeronautics and Space Administration :, 1962), by James R. Johnston, John H. Sinclair, Charles A. Gyorgak, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Effect of impingement angle on drop-size distribution abd spray pattern of two impinging water jets (National Aeronautics and Space Administration :, 1961), by Marcus F. Heidmann, Hampton H. Foster, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Heat transfer to an electrically conducting fluid flowing in a channel with a transverse magnetic field (National Aeronautics and Space Administration :, 1961), by Morris Perlmutter, Robert Siegel, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Ground and in-flight acoustic and performance characteristics of jet-aircraft exhaust noise supressors (National Aeronautics and Space Administration :, 1961), by Willard D. Coles, William H. Swann, John A Mihaloew, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• A cooled-tube pyrometer with experimental results obtained in a high-temperature gas stream. (National Aeronautics and Space Administration :, 1961), by George E. Glawe, Krause,LLyod N., Robert C. Johnson, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Cold-air investigation of prototype Snap-8 turbine (National Aeronautics and Space Administration :, 1962), by William J. Nusbaum, Donald E. Holeski, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Measured base pressures on several twin rocket-nozzle configurations at mach nubmers of 0.6 to 1.4 with effects due to nozzle canting and stabilizing fins (National Aeronautics and Space Administration :, 1960), by James M. Cubbage, Earl H. Andrews, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Experimental investigation of an air-cooled turbine operating in a turbojet engine at turbine inlet temperatures up to 2500 degrees F (National Aeronautics and Space Administration :, 1961), by Reeves P. Cochran, Robert P. Dengler, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Determination of local experimental heat-transfer coefficients on combustion side of an ammonia-oxygen rocket (National Aeronautics and Space Administration :, 1961), by Curt H. Liebert and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Recombination of hydrogen-air combustion products in an exhaust nozzle (National Aeronautics and Space Administration :, 1961), by Erwin A. Lezberg, Richard B. Lancashire, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Annular internal-external-expansion rocket nozzles for large booster applications (National Aeronautics and Space Administration :, 1961), by James F. Connors, Glenn A. Mitchell, Robert W. Cubbison, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Effect of geometric parameters on the static performance of an annular nozzle with a concave central base (National Aeronautics and Space Administration :, 1962), by Charles E. Mercer, Albert J. Simonson, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Transonic performance characteristics of several jet noise suppressors (National Aeronautics and Space Administration :, 1960), by James W. Schmeer, Marlowe D. Cassetti, Leland B. Salters, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Experimental study of combined forced and free-laminar convection in a vertical tube (National Aeronautics and Space Administration :, 1961), by Theodore M. Hallman and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Investigation of the performance of an axial-flow-pump stage designed by the blade-element theory - blade-element data (National Aeronautics and Space Administration :, 1961), by James E. Crouse, John C. Montgomery, Richard F. Soltis, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Nonviscous flow through a pump impeller on a blade-to-blade surface of revolution (National Aeronautics and Space Administration :, 1962), by James J. Kramer, Ralph J. Bean, Norbert O. Stockman, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Potential-flow analysis of unsteady outflow from a tank and its effect on the dynamics of a fluid system (National Aeronautics and Space Administration :, 1962), by William H. Roudebush, I. Irving Pinkel, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Analysis of heat transfer and pressure drop for a gas flowing through a set of multiple parallel flat plates at high temperatures (National Aeronautics and Space Administration :, 1961), by Thomas H. Einstein and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Design and calibration of an arc-heated, hypersonic, low-density wind tunnel (National Aeronautics and Space Administration :, 1962), by Ruth N. Weitmann and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Investigation of the performance of a 78 degree flat-plate helical inducer (National Aeronautics and Space Administration :, 1962), by Richard F. Soltis, Donald M. Sandercock, Douglas A. Anderson, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Experimental study of effects of geometric variables on performance of contoured rocket engine exhaust nozzles (National Aeronautics and Space Administration :, 1962), by Harry E. bloomer, Paul E. Renas, Robert J. Antl, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Incompressible nonviscous blade-to-blade flow through a pump rotor with splitter vanes (National Aeronautics and Space Administration :, 1962), by James J. Kramer, Ralph J. Bean, Norbert O. Stockman, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Effects of suction boundary-layer control on the performance of a short annular diffuser with an upstream terminal normal shock (National Aeronautics and Space Administration :, 1962), by Charles J. Shoemaker, John R. Henry, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Experimental study of effects of geometric variables on performance of conical rocket - engine exhaust nozzles. (National Aeronautics and Space Administration :, 1961), by Harry E. Bloomer, Pqul E. Renas, Robert J. Antl, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Transient temperature profiles and calculated thermal strains of turbojet-engine buckets. (National Aeronautics and Space Administration :, 1961), by J. R. Johnston, R. A. Signorelli, John C. Freche, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Transfer of cryogenic fluids by an expulsion-bag technique. (National Aeronautics and Space Administration :, 1961), by Paul J. Sirocky and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Investigation of an axisymmetric internal compression inlet at a mach number of about 3.8 (National Aeronautics and Space Administration :, 1961), by John H. Lundell, Lewis A. Anderson, Richard Scherrer, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Effects of boattailing and nozzle extension on the thrust-minus-drag of a multiple-jet configuration. (National Aeronautics and Space Administration :, 1961), by William R. Scott and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Experimental performance of nozzles having area ratios up to 300 on JP-4 fuel - liquid-oxygen rocket engine. (National Aeronautics and Space Administration :, 1961), by J. Calvin Lovell, Nick E. Samanich, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Combined effect of contraction ratio and chamber pressure on the performance of a gaseous hydrogen liquid oxygen combustor for a given propellant weight flow and oxidant fuel ratio (National Aeronautics and Space Administration :, 1961), by Martin Hersch and United States National Aeronautics and Space Administration (page images at HathiTrust)
• An investigation to determine the discharge and thrust characteristics of auxiliary-air outlets for a stream Mach number of 3.25 (National Aeronautics and Space Administration :, 1962), by Allen R. Vick and United States National Aeronautics and Space Administration (page images at HathiTrust)
• An Empirical correlation of critical boiling heat flux in forced flow upward through uniformly heated tubes Uwe H. von Glahn. (National Aeronautics and Space Administration :, 1962), by Uwe H. von Glahn and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Effect of afterbody ejection configurations on the performance at transonic speeds of a pylon-supported Nacelle model having a hot-jet exhaust (National Aeronautics and Space Administration :, 1962), by John M. Swihart, Harry T. Norton, Charles E. Mercer, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Combustion instability limits determined by a nonlinear theory and a one-dimensional model / by Richard J. Priem and Donald C. Guentert. (National Aeronautics and Space Administration :, 1962), by Richard J. Priem, Donald C. Guentert, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Surface-temperature distribution on thin-walled bodies subjected to solar radiation in interplanetary space (National Aeronautics and Space Administration :, 1961), by Lester D. Nichols and United States National Aeronautics and Space Administration (page images at HathiTrust)

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