Propulsion systems, theorySee also what's at your library, or elsewhere.
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Filed under: Propulsion systems, theory Calculation procedure for the thermodynamic, transport, and flow properties of the combustion products of a hydrocarbon fuel mixture burned in air with results for ethylene-air and methane-air mixtures / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by E. W. Leyhe, R. R. Howell, and United States National Aeronautics and Space Administration (page images at HathiTrust) An analytical approach to the design of an automatic discontinuous control system / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce, [1961]), by Lawrence W. Taylor, John W. Smith, and United States National Aeronautics and Space Administration (page images at HathiTrust) Theoretical performance of propellants suitable for electrothermal jet engines / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by John R. Jack and United States National Aeronautics and Space Administration (page images at HathiTrust) Ignition of hydrogen-oxygen rocket combustor with chlorine trifluoride and triethylaluminum / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by John W. Gregory, David M. Straight, and United States National Aeronautics and Space Administration (page images at HathiTrust) Emission spectra from high-pressure hydrogen-oxygen combustion / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce, 1962]), by Marshall C. Burrows, Louis A. Povinelli, and United States National Aeronautics and Space Administration (page images at HathiTrust) Recombination of hydrogen-air combustion products in an exhaust nozzle / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by Erwin A. Lezberg, Richard B. Lancashire, 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 / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by Charles E. Mercer, Albert J. Simonson, and United States National Aeronautics and Space Administration (page images at HathiTrust) Analysis of two thrusting techniques for soft lunar landings starting from a 50-mile altitude circular orbit / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962]), by M. J. Queijo, G. Kimball Miller, and United States National Aeronautics and Space Administration (page images at HathiTrust) Numerical solution of two-dimensional Possion equation : Theory and application to electrostatic-ion-engine analysis / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce, 1962]), by Vladimir Hamza, Edward A. Richley, and United States National Aeronautics and Space Administration (page images at HathiTrust) Examination of pressure oscillations induced by changes in the burning rate of flames / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce, [1961]), by Rose L. Schalla and United States National Aeronautics and Space Administration (page images at HathiTrust) Simulations least-squares approximation of a function and its first integrals with application to thermodynamic data. / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by Frank J. Zeleznik, Sanford Gordon, and United States National Aeronautics and Space Administration (page images at HathiTrust) Effect of nozzle convergence length on performance of a heptane-oxygen combustor / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1960]), by Marshall C. Burrows 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 / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by Marcus F. Heidmann, Hampton H. Foster, and United States National Aeronautics and Space Administration (page images at HathiTrust) Propagation of free flames in laminar- and turbulent-flow fields / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1960]), by Ray E. Bolz, Henry Burlage, 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 / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by Martin Hersch and United States National Aeronautics and Space Administration (page images at HathiTrust)
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