Publish Year Decade: 1950 - 1959 / Catalog Issue Year Decade: 1960 - 1969 - Blacklight Search Results

Start Over Publish Year Decade 1950 - 1959 Catalog Issue Year Decade 1960 - 1969

511. 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.)

512. Table of irreducible polynomials over GF(2) through degree 19; [compiled by] Richard W. Marsh

Corporate/Agency Authors:: Business and Defense Services Administration and Commerce Dept.
Publisher:: Business and Defense Services Administration
Date:: Oct. 24, 1957
SuDoc number:: C 41.2:P 76

513. 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.)

514. 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.)

515. 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.)

516. 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.)

517. NACA research memorandum RM (series). E57H07a. Performance of external-internal compression inlet with abrupt inlet with abrupt internal turning at Mach nos. 3.0 to 2.0 [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. 21, 1957
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

518. International population reports, series P-95. 50. U.S.S.R. population census of 1926, partial evaluation [with bibliography]; by John P. Kantner and Lydia W. Kulchycka.

Corporate/Agency Authors:: Census Bureau and Commerce Dept.
Publisher:: Census Bureau
Date:: Oct. 20, 1957
SuDoc number:: C 3.186:P-95/(nos.)

519. NACA research memorandum RM (series). L57G31. Behavior of beryllium and beryllium copper in a 4,000° F supersonic air jet at Mach number of 2 [with list of references]; by William H. Kinard.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Oct. 16, 1957
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

520. NACA research memorandum RM (series). L57I04. Transonic wind-tunnel investigation of low-lift aerodynamic characteristics, including effects of leading-edge droop and thickness, of thin trape-zoidal wing in combination with basic and indented bodies [with list of references]; by Thomas C. Kelly.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Oct. 16, 1957
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

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