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

431. NACA research memorandum RM (series). A57K01. Wind-tunnel investigation of use of leading-edge and trailing-edge area-suction flaps on 13-percent-thick straight wing and fuselage model [with list of references]; by Curt A. Holzhauser.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Jan. 24, 1958
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

432. NACA research memorandum RM (series). L57J28. Free-flight roll performance of steady-flow jet-spoiler control on 80° delta-wing missile between Mach numbers 0.6 and 1.8 [with list of references]; by Eugene D. Schult.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Jan. 24, 1958
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

433. NACA research memorandum RM (series). L57L03. Heat-transfer measurements in free flight at Mach numbers up to 14.6 on flat-faced conical nose with total angle of 29° [with list of references]; by Charles B. Rumsey and Dorothy B. Lee.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Jan. 24, 1958
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

434. NACA research memorandum RM (series). A57J15. Static stability and control of canard configurations at Mach numbers from 0.70 to 2.22, longitudinal characteristics of triangular wing and canard [with list of references]: by John W. Boyd and Victor L. Peterson.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Jan. 22, 1958
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

435. NACA research memorandum RM (series). H57J30. Simulator Investigation of factors affecting design and utilization of stick pusher for prevention of airplane pitch-up [with list of references]; by Euclid C. Holleman and David L. Boslaugh.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Jan. 22, 1958
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

436. NACA research memorandum RM (series). L57I27. Initial experimental study of effect of variations in frequency and impulse on reduction in temperature recovery factor afforded by large-scale unsteady flow [with list of references]; by Robert R. Howell.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Jan. 22, 1958
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

437. NACA research memorandum RM (series). L57J10. Measurements of aerodynamic heat transfer on 15° cone-cylinder-flare configuration in free flight at Mach numbers up to 4.7 [with list of references]: by Charles R. Rumsey and Dorothy B. Lee.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Jan. 22, 1958
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

438. Reports (1957). 1313. Errata [Exploratory investigation of boundary-layer transition on hollow cylinder at Mach number of 6.9], by Mitchel H. Bertram.

Corporate/Agency Authors:: National Advisory Committee for Aeronautics
Publisher:: National Advisory Committee for Aeronautics
Date:: [Jan. 22, 1958]
SuDoc number:: Y 3.N 21/5:5/1313/errata

439. NACA research memorandums RM (series). A57J01. Tracking performance of swept-wing fighter with director-type radar fire-control system and scope presentation [with list of references]; by Howard L. Turner, George A. Rathert, jr., and Donovan R. Heinle.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Jan. 20, 1958
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

440. Research memorandum RM (series). L57J15. Low-speed boundary-layer-control investigation on thin rectangular semispan wing with leading-edge and trailing-edge flaps [with list of references]; by Delwin R. Croon and Thomas R. Turner.

Corporate/Agency Authors:: National Advisory Committee for Aeronautics
Publisher:: National Advisory Committee for Aeronautics
Date:: Jan. 20, 1958
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

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