Catalog Issue Year Decade: 1960 - 1969 / Sudoc Stem: Y 3.N 21/5 - Blacklight Search Results

Start Over Catalog Issue Year Decade 1960 - 1969 Sudoc Stem Y 3.N 21/5

131. NACA research memorandum RM (series). E57K26. Aerodynamic and inlet-flow-field characteristics at free-stream Mach numher of 3.0 for airplanes with circular fuselage cross sections [with list of references]; by Murray Dryer and Roger W. Luidens.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Mar. 18, 1958
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

132. NACA research memorandum RM (series). L57L10. Calculation of flutter characteristics for finite-span swept or onswept wines at subsonic and supersonic speeds by modified strip analysis (with list of references]; by E. Carson Yates, jr.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Mar. 18, 1958
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

133. NACA research memorandum RM (series). L58A22. Preliminary investigation of land-water operation with 1/10-scale model of jet airplane equipped with hydro-skis [with one reference]; by William C. Thompson.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Mar. 18, 1958
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

134. NACA research memorandum RM (series). A57K21. Analog study of influence of internal modifications to wing leading edge on its transient temperature rise during high-speed flight [with list of references]; by Carr B. Neel.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Mar. 17, 1958
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

135. NACA research memorandum RM (series). L58A02. Two-dimensional cascade investigation at Mach numbers up to 1.0 of NACA 65-series blade sections at conditions typical of compressor tips [with list of references]; by James C. Dunavant and James C. Emery.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Mar. 17, 1958
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

136. NACA research memorandum RM (series). L58A03. Section thrust coefficients for full-scale, 3 blade, supersonic-type propeller operating at low and negative blade angles [with list of references]; by Leland B. Salters, jr., and Martha C Lewis.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Washington, Mar. 17, 1958
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

137. NACA research memorandum RM (series). A58A08. Experimental lift-drag ratios for 2 families of wing-body combinations at supersonic speeds [with list of references]; by Leland H. Jorgensen.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Mar. 10, 1958
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

138. NACA research memorandum RM (series). L58A20. Longitudinal and lateral stability and control characteristics at Mach no. 2.01 of 60° delta-wing airplane configuration equipped with canard control and with wing tralling-edge flap controls [with list of references]; by M. Leroy Spearman and Cornelius Driver.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Mar. 10, 1958
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

139. NACA research memorandum RM (series). H58A03a. Flight evaluation of effects of leading-edge-slat span on stability and control characteristics of swept-wing tighter-type airplane during accelerated longitudinal maneuvers at transonic speeds [with list of references]; by Gene J. Matranga and Katherine H. Armistead.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Mar. 6, 1958
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

140. NACA research memorandum RM (series). L57L17a. Effects of canard surface size on stability and control characteristics of 2 canard airplane configurations at Mach nos. 1.41 and 2.01 [with list of references]; by M. Leroy Spearman and Cornelius Driver.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Mar. 6, 1958
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

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