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

641. NACA research memorandum KM (series). E51I07. Effects of Internal configuration on afterburner shell temperatures [with list of references]; by E. William Conrad and Emmert T. Jansen.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Jan. 8, 1952
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

642. NACA research memorandum RM (series). E51I13. Altitude wind tunnel Investigation of performance of compressor, combustor, and turbine components of prototype J47D (RX1-1) turbojet engine [with list of references]; by John M. Farley.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Dec. 21, 1951
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

643. NACA research memorandum RM (series). E51J04. Full-scale investigation of cooling shroud and ejector nossle for turbojet engine-afterburner installation [with list of references]; by Lewis E. Wallner and Emmert T. Jansen.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Dec. 17, 1951
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

644. NACA research memorandum RM (series). E51I04. Investigation of liquid fluorine-liquid diborane propellant combination in 100-pound-thrust rocket engine [with list of references]; by Paul M. Ordin, Howard W. Douglass, and William H. Rowe.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Nov. 30, 1951
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

645. NACA research memorandums RM (series). E51E01. Performance characteristics of aircraft cooling ejectors having short cylindrical shrouds [with list of references]; by Fred D. Kochendorfer and Morris D. Rousso.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: May 22, 1951
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

646. NACA research memorandum RM (series). A51C08. Wind-tunnel investigation at Mach numbers of 1.5 and 2.0 of canard missile configuration [with list of references]; by J. Richard Spabr and Robert A. Robinson.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: May 11, 1951
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

647. NACA research memorandum RM (series). (National Advisory Committee for Aeronautics.) [Processed. No longer confidential.]. L50G07. Langley 9-inch supersonic tunnel tests of several modifications of supersonic missile having tandem cruciform lifting surfaces: Three-component data results of models having ratios of wing span to tall span equal to and less than 1 and some static rolling-moment data [with one reference]; by Robert W. Rainey.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Mar. 7, 1951
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

648. NACA research memorandum RM (series). (National Advisory Committee for Aeronautics.) [Processed. No longer confidential.]. L50I29a. Langley 9-inch supersonic tunnel test of several modifications of supersonic missile having tandem cruciform lifting surfaces: Three-component data results of models having ratios of wing span to tail span less than 1 [with list of references]; by Robert W. Rainey.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Washington, Mar. 7, 1951
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

649. NACA research memorandum RM (series). L9L30. Langley 9-inch supersonic tunnel tests of several modifications of supersonic missile having tandem cruciform lifting surfaces, 3-component data results of models having ratios of wing span to tail span equal to 1; by Robert W. Rainey.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Mar. 7, 1951
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

650. NACA research memorandum RM (series). A50H10. Lateral-control characteristics and dihedral effect of wing-body combination with variable-incidence triangular wing and wing-tip ailerons at Mach number of 1.52 [with list of references]; by Richard Scherrer and David H. Dennis.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Jan. 10, 1951
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

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