Publish Year Decade: 1950 - 1959 / Catalog Issue Year Decade: 1960 - 1969 - Blacklight Search Results

Start Over Publish Year Decade 1950 - 1959 Catalog Issue Year Decade 1960 - 1969

1061. NACA research memorandum RM (series). A52J30. Wind-tunnel investigation at subsonic and supersonic speeds of model of tailless fighter airplane employing low-aspect-ratio swept-back wing-stability and control [with list of references]; by Willard G. Smith.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Jan. 12, 1953
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

1062. NACA research memorandum RM (series). E52J14. Effects of fuel temperature and fuel distribution on combustion efficiency of 16-inch ram-jet engine at simulated flight Mach number of 2.9 [with list of references]; by E. E. Dangle, A. J. Cervenka, and D. W. Bahr.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Jan. 8, 1953
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

1063. Machine gun, history, evolution, and development of manual, automatic, and airborne repeating weapons; compiled by George M. Chinn.

Corporate/Agency Authors:: Naval Weapons Bureau and Defense Dept.
Publisher:: Naval Weapons Bureau
Date:: 1953 [published 1954]
SuDoc number:: D 215.2:M 18/v.3

1064. [Information leaflets] SIL (series). 14. Memorandum regarding obtaining and caring for flying squirrels.

Corporate/Agency Authors:: Smithsonian Institution
Publisher:: Smithsonian Institution
Date:: [Jan. 1953.]
SuDoc number:: SI 1.19:(nos.)

1065. NACA research memorandum RM (series). L52K03. Flight test of radial-burning solid-fuel ram jet [with list of references]; by Walter A. Bartlett, jr., and H. Rudolph Dettwyler.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Dec. 10, 1952
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

1066. NACA research memorandum RM (series). A52I30. Comparison between prediction and experiment for all-movable wing and body combinations at supersonic speeds, drag due to lift and lift-drag ratio [with list of references]; by Elliott D. Katzen and William C. Pitts.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Dec. 5, 1952
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

1067. NACA research memorandum RM (series). L52I19. Evaluation of endand radial-burning solid fuels in ram jets mounted in free Jet at Mach numbers of 2.0, 2.2. and 2.3 [with list of references]; by Walter A. Bartlett, jr.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Nov. 25, 1952
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

1068. NACA research memorandum RM (series). E52H13. Investigation of turbines suitable for use in turbojet engine with high compressor pressure ratio and low compressor-tip speed: 4, Effect of increasing blade speed on velocity diagrams of turbine for engine operation at constant rotative speed [with list of references]; by Elmer H. Davison and Robert E. English.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Nov. 24, 1952
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

1069. NACA research memorandum RM (series). E52G15. Investigation of turbines suitable for use in turbojet engine with high compressor pressure ratio and low compressor-tip speed: 3, Velocity diagram study of 2-stage and downstream-stator turbines for engine operation at constant rotative speed [with list of references]; by Robert E. English and Elmer H. Davison.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Nov. 21, 1952
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

1070. NACA research memorandum RM (series). E52I30. Force and pressure-recovery characteristics of conical-type nose Inlet operating at Mach numbers 1.6 to 2.0 and at angles of attack to 9° [with one reference]: by Andrew Beke and J. L. Allen

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Nov. 19, 1952
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

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