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Performance prediction

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• On bi-grid local mode analysis of solution techniques for 3-D Euler and Navier-Stokes equations (National Aeronautics and Space Administration, Lewis Research Center, Institute for Computational Mechanics in Propulsion ;, 1994), by S. O. Ibraheem, A. O. Demuren, and Lewis Research Center. Institute for Computational Mechanics in Propulsion (page images at HathiTrust)
• General method for predicting efficiency of paraboloidal solar collector (National Aeronautics and Space Administration ;, 1966), by Gabriel N. Kaykaty and Lewis Research Center (page images at HathiTrust)
• Analytical prediction of the performance and stability of a J85-13 compressor with distorted inlet flow (National Aeronautics and Space Administration ;, 1977), by Edward J. Milner and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Cavitation in liquid cryogens. IV, Combined correlations for venturi, hydrofoil, ogives, and pumps (National Aeronautics and Space Administration ;, 1974), by J. Hord, Lewis Research Center, and National Bureau of Standards (page images at HathiTrust)
• Theoretical study of ducted fan performance (National Aeronautics and Space Administration ;, 1970), by M. R. Mendenhall, Selden B. Spangler, Ames Research Center, and Nielsen Engineering & Research (page images at HathiTrust)
• A computer program for the prediction of ducted fan performance (National Aeronautics and Space Administration ;, 1970), by M. R. Mendenhall, Selden B. Spangler, Ames Research Center, and Nielsen Engineering & Research (page images at HathiTrust)
• Experimental investigation of a 4 1/2-stage turbine with very high stage loading factor (National Aeronautics and Space Administration ;, 1973), by D. C. Evans, Lewis Research Center, and General Electric Company (page images at HathiTrust)
• Radio/optical/strapdown inertial guidance study for advanced kick-stage applications. Volume I, Summary. (National Aeronautics and Space Administration ;, 1969), by TRW Inc and Electronics Research Center (U.S.) (page images at HathiTrust)
• High-velocity explosively driven guns (National Aeronautics and Space Administration ;, 1970), by J. D. Watson, Ames Research Center, and Physics International Company (page images at HathiTrust)
• XB-70 flight test data comparisons with simulation predictions of inlet unstart and buzz (National Aeronautics and Space Administration ;, 1970), by Arnold W. Martin, Warren D. Beaulieu, Flight Research Center (U.S.), and North American Rockwell Corporation (page images at HathiTrust)
• Analysis and testing of high entrainment single nozzle jet pumps with variable mixing tubes (National Aeronautics and Space Administration ;, 1972), by Kenneth E. Hickman, Gerald B. Gilbert, Philip G. Hill, Langley Research Center, and Dynatech R/D Company (page images at HathiTrust)
• An approximate method for calculating surface pressures on curved profile blunt plates in hypersonic flow (National Aeronautics and Space Administration, 1959), by Marcus O. Creager and Ames Research Center (page images at HathiTrust)
• Full-scale wind-tunnel investigation of the effects of a target-type thrust reverser on the low-speed aerodynamic characteristics of a single-engine jet airplane (National Aeronautics and Space Administration, 1959), by William H. Tolhurst, Richard K. Greif, Mark W. Kelly, and Ames Research Center (page images at HathiTrust)
• An optimization study of effects on aircraft performance of various forms of heat addition (National Aeronautics and Space Administration, 1960), by Barrett S. Baldwin and Ames Research Center (page images at HathiTrust)
• Analysis of one-dimensional ion rocket with grid neutralization (National Aeronautics and Space Administration, 1960), by Harold Mirels, Burt M. Rosenbaum, and Lewis Research Center (page images at HathiTrust)
• Dynamic analysis of a simple reentry maneuver for a lifting satellite (National Aeronautics and Space Administration, 1959), by Frederick C. Grant and Langley Research Center (page images at HathiTrust)
• Method for predicting off-design performance of axial-flow compressor blade rows (National Aeronautics and Space Administration, 1959), by G. K. Serovy, E. W. Anderson, and Iowa State College (page images at HathiTrust)
• A general method for automatic computation of equilibrium compositions and theoretical rocket performance of propellants (National Aeronautics and Space Administration, 1959), by Sanford Gordon, Vearl N. Huff, Frank J. Zeleznik, and Lewis Research Center (page images at HathiTrust)
• Measured and theoretical flow fields behind a rectangular and a triangular wing up to high angles of attack at a Mach number of 2.46 (National Aeronautics and Space Administration, 1959), by Frank J. Centolanzi and Ames Research Center (page images at HathiTrust)
• A note on the calculation of helicopter performance at high tip-speed ratios (National Aeronautics and Space Administration, 1959), by Alfred Gessow and Langley Research Center (page images at HathiTrust)
• An experimental investigation of the effect of wind tunnel walls on the aerodynamic performance of a helicopter rotor (National Aeronautics and Space Administration, 1960), by Victor M. Ganzer, William H. Rae, and University of Washington (page images at HathiTrust)
• Investigation of methods for computing flutter characteristics of supersonic delta wings and comparison with experimental data (National Aeronautics and Space Administration, 1959), by Charles H. Wilts and California Institute of Technology (page images at HathiTrust)
• Theoretical flow field calculations for project ram (National Aeronautics and Space Administration ;, 1969), by H. Webb, North American Rockwell Corporation, and Langley Research Center (page images at HathiTrust)

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