Publish Year Decade: 1950 - 1959 / Sudoc Stem: Y 3.N 21/5 - Blacklight Search Results

Start Over Publish Year Decade 1950 - 1959 Sudoc Stem Y 3.N 21/5

611. NACA research memorandum RM (series). L57H01. Tests of aerodynamically heated multiweb wing structures in free jet at Mach no. 2, three aluminum-alloy models and one steel model of 20-inch chord and span with various internal structures and skin thicknesses [with list of references]; by Richard Rosecrans, Louis F. Vosteen, and William J. Batdorf, jr.

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.)

612. NACA research memorandum RM (series). L57H19. Tests of aerodynamically heated multiweb wing structures in free jet at Mach no. 2, two aluminum-alloy models of 20-inch chord with 0.064-inch-thick skin at angles of attack of 0° and ±2° [with list of references]; by Georgene H. Miltonberger, George E. Griffith, and John R. Davidson.

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.)

613. 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.)

614. Technical notes. 3176. Errata [Wall Interference in wind tunnels with slotted and porous boundaries at subsonic speeds], by Barrett S. Baldwin, jr., John B. Turner, and Earl D. Knechtel, May 1954.

Corporate/Agency Authors:: National Advisory Committee for Aeronautics
Publisher:: National Advisory Committee for Aeronautics
Date:: [Oct. 25, 1957.]
SuDoc number:: Y 3.N 21/5:6/(nos.)

615. 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.)

616. 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.)

617. 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.)

618. Technical notes. 3433. Errata [Total lift and pitching moment on thin arrowhead wings oscillating in supersonic potential flow], by H. J. Cunningham, May 1955.

Corporate/Agency Authors:: National Advisory Committee for Aeronautics
Publisher:: National Advisory Committee for Aeronautics
Date:: [Oct. 23, 1957]
SuDoc number:: Y 3.N 21/5:6/(nos.)

619. 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.)

620. 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.)

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