Author: National Aeronautics and Space Administration / Publish Year Decade: 1950 - 1959 - Blacklight Search Results

Start Over Author National Aeronautics and Space Administration Publish Year Decade 1950 - 1959

561. NACA research memorandum RM (series). L56I27. Transonic flutter investigation of two 64° delta wings with simulated streamwise rib and orthogonal spar construction [with list of references]; by George W. Jones, jr., and Lou S. Young, jr.

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

562. NACA research memorandum RM (series). A56K07. Simplified method for assessing effect of steady rolling on angle of attack and sideslip [with list of references]; by Stanley F. Schmidt [and others]. Washington, Jan.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: 17, 1957
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

563. NACA research memorandum RM (series). E57F13b. Analytical study of equilibrium thickness of boric oxide deposits on jet-engine surfaces [with list of references]; by Paul C. Setze. Washington, Oct. 8.

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

564. NACA research memorandum RM (series). L56I13. Investigation of static pressures and boundary-layer characteristics on forward parts of 9 fuselages of various cross-sectional shapes at Moo=2.01 [with list of references]; by Lowell E. Hasel and Walter L. Kouyoumjian.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Jan. 1, 1957
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

565. NACA research memorandum RM (series). L56J17. Hinge-moment and effectiveness characteristics of aspect-ratio-8.2 flap-type control on 60° delta wing at Mach numbers from 0.72 to 1.96 [with list of references]; by Lawrence D. Guy.

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

566. NACA research memorandum RM (series). E56B14. Component performance of J71-A-2 (600-D1) turbojet engine at several Reynolds number indices [with list of references]; by Ferris L. Seashore and Lester C. Corrington.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Dec. 28, 1956
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

567. NACA research memorandum RM (series). E56B16. Altitude performance of J71-A-2(600-D1) turbojet engine [with list of references]; by Ivan D. Smith and Joseph N. Sivo.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Dec. 28, 1956
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

568. NACA research memorandum RM (series). E56I21. Evaluation of liquefied hydrocarbon gases as turbojet fuels [with list of references]; by Robert R. Hibbard.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Dec. 28, 1956
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

569. NACA research memorandum RM (series). L56I14. Experimental study and analysis of loading and pressure distributions on delta wings due to thickness and to angle of attack at supersonic speeds [with list ol references]; by William B. Boatright.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Dec. 26, 1956
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

570. NACA research memorandum RM (series). L56J31a. Wind-tunnel investigation of effects of ventral fins at 2 positions on lateral-stability derivatives of 45° swept high-wing model oscillating in yaw [with list of references]; by Byron M. Jaquet.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Dec. 26, 1956
SuDoc number:: Y 3.N 21/5:15/(letters-nos.)

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