Author: National Aeronautics and Space Administration / Sudoc Stem: Y 3.N 21/5 - Blacklight Search Results

Start Over Author National Aeronautics and Space Administration Sudoc Stem Y 3.N 21/5

1111. NACA research memorandum RM (series). E54C23. Performance of wedge-type boundary layer diverters for side inlets at supersonic speeds [with list of references]; by Robert C. Campbell and Emil J. Kremzier.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: May 13, 1954
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

1112. NACA research memorandum RM (series). E53L28. Effect of inlet-annulus area blockage on over-all performance and stall characteristics of experimental 15-stage axial-flow compressor [with list of references]; by James G. Lucas, Harold B. Finger, and Richard E. Filippi.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: May 11, 1954
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

1113. NACA research memorandum RM (series). A54B0S. Effect of lip shape on nose-inlet installation at Mach numbers from 0 to 1.5 and method for optimizing engine-inlet combinations [with list of references]; by Emmet A. Mossman and Warren E. Anderson.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: May 7, 1954
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

1114. NACA research memorandum RM (series). E54B11. Aerodynamics of slender bodies at Mach number 3.12 and Reynolds numbers from 2×106 to 15×106: 5, Aerodynamic load distributions for series of 4 boattailed bodies [with list of references]; by Barry Moskowitz and John R. Jack.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: May 6, 1954
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

1115. NACA research memorandum RM (series). E54B24. Performance of isentropic nose inlets at Mach number of 5.6 [with list of references]; by Harry Bernstein and Rudolph C. Haefell.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: May 6, 1954
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

1116. NACA research memorandum RM (series). A54C04. Experimental investigation of aerodynamic characteristics of ballistictype missile [with list of references]; by Stanford E. Neice.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Apr. 23, 1954
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

1117. NACA research memorandum RM (series). A54B15a. Experimental Investigation of damping in roll of cruciform triangular wing-body combinations at Mach numbers from 1.5 to 6.0 [with list of references]; by Alfred G. Bolssevaln.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Apr. 7, 1954
SuDoc number:: Y 3.N 21/5:15/(letters-nos.)

1118. NACA research memorandum RM (series). L53I30. Aerodynamic load measurements and opening characteristics of automatic leading-edge slats on 45° sweptback wing at transonic speeds [with list of references]; by Donald D. Arabian, Jack F. Runckel, and Charles F. Reid, jr.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Apr. 7, 1954
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

1119. NACA research memorandum RM (series). E54A21. Analysis of turbojet engine for propulsion of supersonic bombers [with list of references]; by Richard P. Krebs and E. Clinton Wilcox.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Apr. 5, 1954
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

1120. NACA research memorandum RM (series). L53J08. Aerodynamic characteristics at transonic speeds of model with 45° sweptback wing, including effect of leading-edge slats and low horizontal tail [with list of references]; by Jack F. Runckel and James W. Schmeer.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Apr. 5, 1954
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

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