Publisher: National Aeronautics and Space Administration / Publish Year Decade: 1950 - 1959 - Blacklight Search Results

Start Over Publisher National Aeronautics and Space Administration Publish Year Decade 1950 - 1959

1161. NACA research memorandum RM (series). E52I10. Effect of rotorand stator-blade modifications on surge performance of 11-stage axial-flow compressor: 2, redesigned compressor for XJ40-WE-6 engine [with list of references]; by B. William Conrad, Harold B. Finger, and Robert H. Essig.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: May 25, 1953
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

1162. NACA research memorandum RM (series). E52G03. Effect of rotorand stator-blade modifications on surge performance of 11-stage axial flow compressor: 1, Original production compressor of XJ40-WE-6 engine [with list of references]; by Harold B. Finger, Robert H. Essig, and E. William Conrad.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: May 20, 1953
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

1163. NACA research memorandum RM (series). E52J20. Preliminary evaluation of turbine performance with variable-area turbine nozzles in turbojet engine [with one reference]; by Carl E. Campbell and Harry J. Welna.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: May 20, 1953
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

1164. NACA research memorandum RM (series). E52H18. Matched performance characteristics of 16-stage axial-flow compressor and 3-stage turbine [with list of references]; by John J. Rebeske, jr., and James P. Dugan, jr.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Apr. 28, 1953
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

1165. NACA research memorandum RM (series). E53B16. Use of flame-immersed blades to improve combustion limits and efficiency of 5-inch diameter connected-pipe, ram-jet combustor [with list of references]; by Donald W. Male.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Apr. 9, 1953
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

1166. NACA research memorandum RM (series). L53A16a. Note on drag due to lift of delta wings at Mach numbers up to 2.0 [with list of references]; by Robert S. Osborne and Thomas C. Kelly.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Apr. 9, 1953
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

1167. NACA research memorandum RM (series). L53B09. Effects of span and spanwise and chordwise location on control effectiveness of spoilers on 50° sweptback wing at Mach numbers of 1.41 and 1.96 [with list of references]; by William H. Kindell.

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

1168. NACA research memorandum RM (series). E53B04. Effect of fuel injectors and liner design on performance of annular turbojet combustor with vapor fuel [with list of references]; by Carl T. Norgren and J. Howard Childs.

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

1169. NACA research memorandum RM (series). E53A28. Effect of axially staged fuel introduction on performance of one-quarter sector of annular turbojet combustor [with list of references]; by Eugene V. Zettle and Herman Mark.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Mar. 30, 1953
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

1170. NACA research memorandum RM (series). L53A27. Low-lift drag and stability data from rocket models of modified-delta-wing airplane with and without external stores at Mach numbers from 0.8 to 1.36 [with list of references]; by Grady L. Mitcham and Willard S. Blanchard, jr.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Mar. 26, 1953
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

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