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

3131. NACA research memorandum RM (series). A52.T31. Wind-tunnel investigation at subsonic and supersonic speeds of model of tailless fighter airplane employing low-aspect-ratio swept-baek wing-effects of external fuel tanks and rocket packets on drag characteristics [with list of references]; by Willard G. Smith.

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

3132. 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.)

3133. 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.)

3134. NACA research memorandum RM (series). L52K10. Preliminary investigation of total-pressure-recovery characteristics of 15° semiangle movable-cone variable-geometry ram-jet inlet at free-jet Mach numbers of 1.62, 2.00, 2.53, and 3.05 [with list of references]; by Arthur H. Hinners, jr., and John B. Lee.

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.)

3135. 38th annual report of National Advisory Committee for Aeronautics, [fiscal year] 1952, administrative report without technical reports.

Corporate/Agency Authors:: National Advisory Committee for Aeronautics
Publisher:: National Advisory Committee for Aeronautics
Date:: 1953
SuDoc number:: Y 3.N 21/5:1/952

3136. NACA research memorandum RM (series). E53B03. Aerodynamics of slender bodies at Mach number 3.12 and Reynolds numbers from 2×106 to 15×10s: 3, Boundary layer and force measurements on slender cone-cylinder body of revolution [with list of references]; by John R. Jack. Washington, Apr.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: 6, 1953
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

3137. NACA research memorandum RM (series). E53G24. Performance of annular turbojet combustor having reduced pressure losses and using propane fuel [with list of references]; by Carl T. Norgren and J. Howard Childs. Washington, Sept.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: 24, 1953
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

3138. Report (1947). 871. Errata no. 2, Determination of elastic stresses in gas-turbine disks; by S. S. Manson, 1947.

Corporate/Agency Authors:: National Advisory Committee for Aeronautics
Publisher:: National Advisory Committee for Aeronautics
Date:: [1953.]
SuDoc number:: Y 3.N 21/5:5/871/errata2

3139. Report (1952). 1069. On a solution of nonlinear differential equation for transonic flow past a wave-shaped wall [with list of references]; by Carl Kaplan.

Corporate/Agency Authors:: National Advisory Committee for Aeronautics
Publisher:: National Advisory Committee for Aeronautics
Date:: [1953.]
SuDoc number:: Y 3.N 21/5:5/(nos.)

3140. Report (1952). 1084. Comparison of high-speed operating characteristics of size 215 cylindrical-roller bearings as determined in turbojet engine and in laboratory test rig [with list of references]; by E. Fred Macks and Zolten N. Nemeth.

Corporate/Agency Authors:: National Advisory Committee for Aeronautics
Publisher:: National Advisory Committee for Aeronautics
Date:: [1953.]
SuDoc number:: Y 3.N 21/5:5/1084

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