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

671. NACA research memorandum RM (series). L57G18. Effect of conical and flat sting-mounted windshields on zero-lift drag of flare-stabilized bluff body at Mach numbers from 0.6 to 1.15 [with list of references]; by Willard S. Blanchard, jr..

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Sept. 12, 1957
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

672. NACA research memorandum RM (series). L57G11. Free-flight investigation of jet effect on low-lift drag and longitudinal trim of supersonic interceptor-type airplane configuration with overhanging tail boom at Mach numbers from 1.09 to 1.34 [with list of references]; by Willard S. Bianchard, jr.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Sept. 10, 1957
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

673. Technical memorandums. 1408. Principles of turbulent heat transfer [with list of references], by H. Reichardt; translation [by S. Reiss].

Corporate/Agency Authors:: National Advisory Committee for Aeronautics
Publisher:: National Advisory Committee for Aeronautics
Date:: Sept. 1957
SuDoc number:: Y 3.N 21/5:8/(nos.)

674. Technical notes. 3585. Determination of surge and stall limits of axial-flow turbojet engine for control applications [with list of references]; by Ross D. Schmidt, George Vasu, and Edward W. McGraw.

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

675. Technical notes. 4032. Reduction of oxidized nichrome V powders and sintering of nichrome V bodies [with list of references]; by Paul Sikora and Philip Clarkin.

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

676. Technical notes. 4039. Investigation of effects of profile shape on aerodynamic and structural characteristics of thin, 2-dimensional airfoils at supersonic speeds [with list of references]; by Elliott D. Katzen, Donald M. Kuehn, and William A. Hill, jr.

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

677. Technical notes. 4063. Equations, tables, and figures for use in analysis of helium flow at supersonic and hypersonic speeds [with bibliography]; by James N. Mueller.

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

678. Technical notes. 4075. Tensile stress strain properties of 17-7 PH and AM 350 stainless steel sheet at elevated temperatures [with list of references]; by Ivo M. Kurg.

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

679. Technical notes. 4076. Calculated and measured stresses in simple panels subject to intense rendom acoustic loading Including near noise field of turbojet engine [with list of references]; by Leslie Lassiter and Robert W. Hess.

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

680. Technical notes. 4077. Static longitudinal and lateral stability characteristics at low speed of 45° swept back-midwing models having wings with aspect ratio of 2, 4 or 6 [with list of references]; by David F. Thomas, jr. and Walter D. Wolhart.

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

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