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

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

661. NACA research memorandum RM (series). H56E02. Lift and drag of Bell X-5 research airplane in 45° sweptback configuration at transonic speeds [with list of references]; by Jack Nugent.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: July 11, 1956
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

662. NACA research memorandum RM (series). L56D04. Static longitudinal stability and control characteristics of model of 45° swept-wing fighter airplane at Mach numbers of 1.41, 1.61, and 2.01 [with list of references]; by Cornelius Driver and Gerald V. Foster.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: July 11, 1956
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

663. NACA research memorandum RM (series). L5GE07. Some experiments relating to problem of simulation of hot jet engines in studies of jet effects on adjacent surface at free-stream Mach number of 1.80 [with list of references]; by Walter E. Bressette.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Washington, July 11, 1956
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

664. NACA research memorandum RM (series). L56D25. Free-flight aerodynamic-heating data to Mach number 10.4 for modified Von Karman nose shape [with list of references]; by William M. Bland, jr., and Katherine A. Collie.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: July 10, 1956
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

665. NACA research memorandum RM (series). L56C05. Turbulent and laminar heat-transfer measurements on ⅛-scale NACA RM-10 missile in free flight to Mach number of 4.2 and to wall temperature of 1400° R [with list of references]; by Robert O. Piland, Katherine A. Collie, and William E. Stoney

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

666. NACA research memorandums RM (series). E56D16. Performance of short turbojet combustor with hydrogen fuel in quarter-annulus duct and comparison with performance in full-scale engine [with list of references]; by Robert Friedman, Cart T. Norgren, and Robert E. Jones.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: July 2, 1956
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

667. NACA research memorandum RM (series). E56D12. Stability of supersonic inlets at Mach 1.91 with air injection and suction [with list of references]; by K. Kowalski and Thomas G. Piercy.

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

668. NACA research memorandum RM (series). E56A13. Preliminary survey of compressor rotor-blade wakes and other How phenomena with hot-wire anemometer; by Theodore E. Fessler and Melvin J. Hartmann.

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

669. NACA research memorandum RM (series). E56C14. External-stream effects on gross thrust and pumping characteristics of ejectors operating at off-design Mach numbers [with list of references]; by Alfred S. Valerino and Richard A. Yeager.

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

670. NACA research memorandum RM (series). A56C06. Change with mass-flow ratio of cowl pressure drag of normal-shock inlets at supersonic speeds [with list of references]: by Wallace F. Davis and Forrest E. Gowen.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: June 22, 1956
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

« Previous
Next »
1
2
…
63
64
65
66
67 Current Page, Page 67
68
69
70
71
…
126
127