Publisher: National Aeronautics and Space Administration - Blacklight Search Results

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17301. NACA research memorandum RM (series). E52E20. Survey of some preliminary investigations of supersonic diffusers at high Mach numbers [with list of references]: by Edgar M. Cortright, jr., and James F. Connors.

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

17302. NACA research memorandum RM (series). E52B29. Over-all performance of J71 3-stage turbine [with one reference]; by William E. Berkey.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: July 9, 1952
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

17303. NACA research memorandum RM (series). E51L07. Altitude wind tunnel Investigation of high-temperature afterburners [with list of references]; by E. William Conrad and Carl E. Campbell.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: June 26, 1952
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

17304. NACA research memorandum RM (series). E52D14. Investigation of turbines suitable for use in turbojet engine with high compressor pressure ratio and low compressor-tip speed: 2, Velocitydiagram study of turbine for engine operation with constant exhaust-nozzle area [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:: June 19, 1952
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

17305. NACA research memorandum RM (series). E52C26. Investigation of internal film cooling of exhaust nozzle of 1000-poundthrust liquid-ammonia liquid-oxygen rocket [with list of references]; by Andrew E. Abramson.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: June 17, 1952
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

17306. NACA research memorandum RM (series). E51L10. Performance of components of XJ34-WE-32 turbojet engine over range of engine and flight conditions [with one reference]; by John E. McAulay, Adam E. Sobolewski, and Ivan D. Smith.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: June 9, 1952
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

17307. NACA research memorandum RM (series). E52A21. Axial-slot air admission for controlling performance of one-quarter-annulus turbojet combustor and comparison with complete engine [with list of references]; by Herman Mark and Eugene V. Zettle.

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

17308. NACA research memorandum RM (series). E52A16. Investigation of turbines suitable for use in turbojet engine with high compressor pressure ratio and low compressor-tip speed: 1, Turbine-design requirements for several engine operating conditions [with list of references]; by Robert E. English, David H. Silvern, and Elmer H. Davison.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Mar. 4, 1952
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

17309. NACA research memorandum RM (series). L51L20. Pressure measurements on ogive-cylinder body at Mach number 4.04 [with list of references]; by Douglas R. Lord and Edward F. Ulmann.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Feb. 26, 1952
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

17310. NACA research memorandum RM (series). L51I28. Rocket-model investigation of rolling effectiveness of fighter-type wingcontrol configuration at Mach numbers from 0.6 to 1.5 [with list of references]; by H. Kurt Strass and Edward T. Marley.

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

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