Author: National Aeronautics and Space Administration / Publish Year Decade: 1950 - 1959 - Blacklight Search Results

Start Over Author National Aeronautics and Space Administration Publish Year Decade 1950 - 1959

881. NACA research memorandum RM (series). E54I28. Steady-state and surge characteristics of compressor equipped with variable inlet guide vanes operating in turbojet engine [with list of references]; by Lewis E. Wallner and Robert J. Lubick.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: June 20, 1955
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

882. NACA research memorandum RM (series). L55D28. Investigation at supersonic speeds of external-drag effects and pumping characteristics of short ejector [with list of references]; by Eugene S. Love and Robert M. O'Donnell.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: June 14, 1955
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

883. NACA research memorandum RM (series). L55E12a. Loads associated with spoilers at supersonic speeds [with list of references]; by Douglas R. Lord and K. R. Czarnecki.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Washington. June 14, 1955
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

884. NACA research memorandum RM (series). E55D05a. Survey of methods for tubojet thrust measurement applicable to flight installations [with list of references]; by William A. Fleming and David S. Gabriel.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: June 10, 1955
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

885. NACA research memorandum RM (series). E54K26a. Effect of circumferential total-pressure gradients typical of singleinlet duct installations on performance of axial-flow turbojet engine [with list of references]; by S. C. Huntley, Joseph N. Sivo, and Curtis L. Walker.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: June 3, 1955
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

886. NACA research memorandum RM (series). L55D13. Experimental investigation of zero-lift wave drag of 7 pairs of delta wings with constant and varying thickness ratios at Mach numbers of 1.62, 1.93, and 2.41 [with list of references]; by Arthur Henderson, jr..

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: June 3, 1955
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

887. NACA research memorandum RM (series). E55A31. Analytic evaluation of effect of inlet-air temperature and combustion pressure on combustion performance of boron slurries and blends of pentaborane in octene-1 [with list of references]; by Leonard K. Tower.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: June 1, 1955
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

888. NACA research memorandum RM (series). E55B28. Investigation of high-pressure-ratio 8-stage axial-flow research compressor with 2 transonic inlet stages: 4, Modification of aerodynamic design and prediction of performance [with list of references]; by Richard P. Geye and Charles H. Voit.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: June 1, 1955
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

889. NACA research memorandum RM (series). E55C07. Experimental evaluation of boron-hydrocarbon slurry in 10-inch ramjet combustor [with list of references]; by William R. Kerslake, E. E. Dangle, and A. J. Cervenka.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: June 1, 1955
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

890. NACA research memorandum RM (series). A55C30a. Effect of wing fences on longitudinal characteristics at Mach numbers up to 0.92 of wing-fuselage-tail combination having 40° swept-back wing with NACA 64A thickness distribution [with list of references]; by Jerald K. Dickson and Fred B. Sutton.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: May 27, 1955
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

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