Author: National Aeronautics and Space Administration / Publisher: National Aeronautics and Space Administration - Blacklight Search Results

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17211. NACA research memorandum RM (series). E53F10. Altitude evaluation of several afterburner design variables on J47-GE-17 turbojet engine [with list of references]: by Willis M. Braithwaite, Curtis L. Walker and Joseph N. Sivo.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Oct. 23, 1953
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

17212. NACA research memorandum RM (series). E53H11. Performance comparison at supersonic speeds of inlets spilling excess flow by means of bow shock, conical shock, or bypass [with list of references]; by J. L. Allen and Andrew Beke.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Oct. 23, 1953
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

17213. NACA research memorandum RM (series). A53H12. Analysis of tracking performances of 2 straight-wing and 2 sweptwing fighter airplanes with fixed sights in standardized test maneuver [with list of references]; by George A. Rathert, jr., Burnett L. Gadeberg.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Oct. 22, 1953
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

17214. NACA research memorandum RM (series). E53H14. Free-jet investigation of 20-inch ram-jet combustor utilizing highheat-release pilot burner fwlth list of references]; by James G. Henzel jr., and Carl B. Wentworth.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Oct. 16, 1953
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

17215. NACA research memorandum RM (series). E53H04. Investigation at Mach numbers 1.5 and 1.7 of twin-duct side air-intake system with 9° compression ramp including modifications to boundarylayer-removal wedges and effects of bypass system [with list of references]; by Leonard J. Obery and Leonard E. Stitt.

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

17216. NACA research memorandum RM (series). E53H19. Investigation at Mach numbers 1.5 and 1.7 of twin-duct side intake system with 2-dimensional 6° compression ramps mounted on supersonic airplane [with one reference]; by Joseph Davids and George A. Wise.

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

17217. NACA research memorandum RM (series). A53H10. Flight study of effects on tracking performance of changes in lateraloscillatory characteristics of fighter airplane [with list of references]; by Walter E. McNeill, Fred J. Drinkwater III, and Rudolph D. Van Dyke, jr.

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

17218. NACA research memorandum RM (series). E53G06. Analysis of turbine stator adjustment required for compressor designpoint operation in high Mach number supersonic turbojet engines [with list of references]; by Robert E. English and Richard H. Cavicchi.

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

17219. NACA research memorandum RM (series). E53H15. Effect of flame-holder design of altitude performance of louveredliner afterburner [with list of references]; by Paul E. Renas and Emmert T. Jansen.

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

17220. NACA research memorandum RM (series). L53I03. Component tests to determine aerodynamic characteristics of allmovable 70° delta canard-type control in presence of body at Mach number of 1.61 [with list of references]; by M. Leroy Spearman.

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

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