Catalog Issue Year Decade: 1960 - 1969 / Sudoc Stem: Y 3.N 21/5 - Blacklight Search Results

Start Over Catalog Issue Year Decade 1960 - 1969 Sudoc Stem Y 3.N 21/5

61. NACA research memorandum RM (series). E58D04a. Experimental performance of 0.35 huh-tip radius ratio transonic axial flow-compressor stage designed for 40 pounds per second per unit frontal area [with list of references]; by Richard R. Cullom, John C. Montgomery, and Paul T. Tasaki.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Sept. 4, 1958
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

62. NACA research memorandum RM (series). E58D17. Design and experimental performance of 0.85 hub-tip radius ratio transonic axial-flow compressor rotor designed for 40 pounds per second per unit frontal area [with list of references]; by John C. Montgomery and Paul T. Yasaki.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Sept. 4, 1958
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

63. NACA research memorandum RM (series). E58E12. Thermal reaction of diborane with trimethylborane [with list of references]; by John H. Lamneck, jr., and Samuel Kayo.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Washington, Sept. 4, 1958
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

64. NACA research memorandum RM (series). E58E20. Comparison of calculated and experimental temperatures and coolant pressures losses for cascade of small air-cooled turbine rotor blades [with list of references]; by Francis S. Stepka.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Sept. 4, 1958
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

65. NACA research memorandum RM (series). A58E19. Experimental investigation of effect of yaw on rates of heat transfer to transverse circular cylinders in 6500-foot-per-second hypersonic air stream [with list of references]: by Bernard E. Cunningham and Samuel Kraus.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Aug. 26, 1958
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

66. NACA research memorandum RM (series). A58E21n. Forces and pitching moments on aspect-ratio-3.1 wing-body combination at Mach numbers from 2.5 to 3.5 and sublimation studies of effect of single-element roughness on boundary-layer flow [with list of references]; by Edward J. Hopkins, Stephen J. Keating, jr., and Richard R. Muhl.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Washington, Aug. 26, 1958
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

67. NACA research memorandum RM (series). L58F26. Investigation of tilting-wing vertical-take-off-and-landing jet airplane model in hovering and transition flight [with list of references]; by Robert H. Kirby and James L. Hassell, jr.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Aug. 26, 1958
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

68. NACA research memorandum RM (series). E58D24. Use of shock-trap bleed to Improve pressure recovery of fixed-andvariable-capture-area internal-contraction inlets, Mach number 2.0 to 8.0 [with list of references]; by Roger W. Luidens and Richard J. Flaherty.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Aug. 14, 1958
SuDoc number:: Y 3.N 21/5:15/(letters-nos.)

69. NACA research memorandum RM (series). L58E26. Longitudinal and lateral aerodynamic characteristics at combined angles of attack and sideslip of generalized missile model having rectangular wing at Mach number of 4.08 [with list of references]; by Fred M. Smith, Edward F. Ulmann, and Robert W. Dunning.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Washington, Aug. 14, 1958
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

70. NACA research memorandum RM (series). L58E29. Wind-tunnel investigation of effect of sweep and taper ratio on effectiveness of spoiler-slot-deflector controls on aspect-ratio 4 wings at transonic speeds [with list of references]; by Alexander D. Hammond and Linwood W. McKinney.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Washington, Aug. 14, 1958
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

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