Publish Year Decade: 1950 - 1959 / Sudoc Stem: Y 3.N 21/5 - Blacklight Search Results

Start Over Publish Year Decade 1950 - 1959 Sudoc Stem Y 3.N 21/5

1811. NACA research memorandum RM (series). E55H31. Performance and component frontal areas of hypothetical 2-spool turbojet engine for 3 modes of operation [with list of references]; by James F. Dugan, jr.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Dec. 19, 1955
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

1812. NACA research memorandum RM (series). E55I26. Preliminary investigation of effect on performance of dividing conicalspike nose inlets into halves at Mach numbers 1.5 to 2.0 [with list of references]; by John L. Allen.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Dec. 19, 1955
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

1813. NACA research memorandum RM (series). E55J17. Turbojet engine investigation of effect of thermal shock induced by external water-spray cooling on turbine blades of 5 high-temperature alloys [with list of references]; by John C. Freche and Robert O. Hickel.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Dec. 19, 1955
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

1814. NACA research memorandum RM (series). E55J20. Rocket-engine throttling [with list of references]; by William A. Tomazic.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Dec. 19, 1955
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

1815. NACA research memorandum RM (series). L55H23. Force and pressure measurements on several canopy-fuselage configurations at Mach numbers 1.41 and 2.01 [with list of references]; by A. Warner Robins.

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

1816. NACA research memorandum RM (series). L55I09. Effect of inlet installation on zero-lift drag of 60° delta-wing-body configuration from flight tests at Mach numbers from 0.8 to 1.86 [with list of references]; by Charles F. Merlet.

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

1817. NACA research memorandum RM (series). L55I12. Lift, drag, and longitudinal stability at Mach numbers from 1.4 to 2.3 of rocket-powered model having 52.5° sweptback wing of aspect ratio 3 and in-line tail surfaces [with list of references]; by Warren Gillespie, jr.

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

1818. NACA research memorandum RM (series). L55I13. Flight investigation of effect of underwing propulsive jets on lift, drag, and longitudinal stability of delta-wing configuration at Mach numbers from 1.23 to 1.62 [with list of references]; by Ralph A. Falanga and Joseph H. Judd.

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

1819. NACA research memorandum RM (series). L55I27a. Origin and distribution of supersonic store interference from measurement of individual forces on several wing-fuselage-store configurations: 4, Delta-wing heavy-bomber configuration with large store, Mach number, 1.61 [with list of references]; by Odell A. Morris.

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

1820. Technical notes. 3529. Transonic characteristics of 36 symmetrical wings of varying taper, aspect ratio, and thickness as determined by transconic-bump technique [with list of references]; by Warren H. Nelson, Edwin C. Allen and Walter J. Krumm.

Corporate/Agency Authors:: National Advisory Committee for Aeronautics
Publisher:: National Advisory Committee for Aeronautics
Date:: Dec. 1955
SuDoc number:: Y 3.N 21/5:6/(nos.)

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