Author: National Aeronautics and Space Administration / Catalog Issue Year Decade: 1960 - 1969 - Blacklight Search Results

Start Over Author National Aeronautics and Space Administration Catalog Issue Year Decade 1960 - 1969

10211. NACA research memorandum RM (series). L57I18. Analog-computer investigation of effects of friction and preload on dynamic longitudinal characteristics of pilot-airplane combination [with list of references]; by Harold L. Crane.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Nov. 20, 1957
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

10212. NACA research memorandum RM (series). E57H07b. Performance of translating-double-cone axisymmetrie inlet with cowl by pass at Mach numbers from 2.0 to 3.5 [with list of references]; by James F. Connors and George A. Wise.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Nov. 13, 1957
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

10213. NACA research memorandum RM (series). E57I19. Investigation of turbines suitable for use in turbojet engine with high compressor pressure ratio and low compressor-tip speed: 8, Internal flow conditions of 2-stage turbine with downstream stator [with list of references]; by Donald A. Petrash, Elmer H. Davison, and Harold J. Schum.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Nov. 13, 1957
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

10214. NACA research memorandum RM (series). L57H22. Transonic flutter Investigation of arrowhead wing with tip ailerons and trailing-edge flaps [with list of references]; by George W. Jones, jr., and Robert W. Boswinkle, jr.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Nov. 4, 1957
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

10215. NACA research memorandum RM (series). A57I10. Effects of vertical location of wing and horizontal tall on aerodynamic characteristics in pitch at Mach numbers from 0.60 to 1.40 of airplane configuration with unswept wing [with list of references]; by Louis S. Stivers, jr., and Garth W. Lippmann.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Nov. 1957
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

10216. NACA research memorandum RM (series). L57I13. Static lateral characteristics at high subsonic speeds of complete airplane model with highly tapered wing having 0.80 chord line unswept and with several tall configurations [with list of references]; by Kenneth W. Goodson.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Oct. 28, 1957
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

10217. NACA research memorandum RM (series). L57G05. Aerodynamic and hydrodynamic characteristics of proposed supersonic multijet water-based hydro-ski aircraft with variable-incidence wing [with list of references]; by William W. Petynia, Dennis F. Hasson, and Stanley H. Spooner.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Oct. 23, 1957
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

10218. NACA research memorandum RM (series). L57H05. Two-dimensional cascade tests of NACA 65-(C10A10 blade sections at typical compressor hub conditions for speeds up to choking [with list of references]; by James C. Emery and James C. Dunavant.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Oct. 23, 1957
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

10219. NACA research memorandum RM (series). L57I03. Preliminary indications of cooling achieved by ejecting water upstream from stagnation point of hemispherical, 80° conical, and flat-faced nose shapes at stagnation temperature of 4,000° F [with one reference]; by Bernard Rashis.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Oct. 23, 1957
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

10220. NACA research memorandum RM (series). E57F10. Free-flight determination of boundary-layer transition and heat transfer for hemisphere-cylinder at Mach numbers to 5.6 [with list of references]; by M. J. Krasnican and R. J. Wisnlewski.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Oct. 21, 1957
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

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