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

691. NACA research memorandum RM (series). L56A18. Transonic investigation of static longitudinal-stability characteristics of 45° sweptback wing-fuselage combination with and without horizontal tail [with list of references]; by Chris C. Critzos.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: May 1, 1956
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

692. NACA research memorandum RM (series). L56B07. Measurements of aerodynamic heat transfer and boundary-layer transition on 10° cone in free flight at supersonic Mach numbers up to 5.9 [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:: Apr. 26, 1956
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

693. NACA research memorandum RM (series). L56B15. Wind-tunnel investigation of damping in roll of Bell X-1E research airplane and its components at supersonic speeds [with list of references]; by Russell W. McDearmon and Frank L. Clark.

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

694. NACA research memorandum RM (series). L56B27. Supersonic-area-rule design and rocket-propelled flight investigation of zero-lift straight-wing-body-nacelle configuration between Mach numbers 0.8 and 1.53 [with list of references]; by Sherwood Hoffman.

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

695. NACA research memorandum RM (series). E55L22. Temperature-control study of turbine region of turbojet engine, including turbine-blade time constants and starting characteristics [with list of references]; by W. E. Phillips, jr.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Apr. 25, 1956
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

696. NACA research memorandum RM (series). E56A24. Design of 2 transpiration-cooled strut-supported turbine rotor blades [with list of references]; by Ernst I. Prasse, John N. B. Livingood, and Patrick L. Donoughe.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Apr. 25, 1956
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

697. NACA research memorandum RM (series). E56B17. Analysis of cooling-air requirements of corrugated-insert-type turbine blades suitable for supersonic turbojet engine [with list of references]; by Robert R. Ziemer and Henry O. Slone.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Apr. 25, 1956
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

698. NACA research memorandum RM (series). E56B20. Analytical investigation of factors affecting performance of single-stage turbines having rotor-tip discharge of cooling air [with list of references]; by Gordon T. Smith and Robert O. Hickel.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Apr. 25, 1956
SuDoc number:: Y 3.N 21/5:15/(letters-nos.)

699. NACA research memorandum RM (series). L56B09. Brief investigation of effect of waves on take-off resistance of seaplane [with list of references]; by Elmo J. Mottard.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Apr. 24, 1956
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

700. NACA research memorandum RM (series). L56A03. Investigation of effects of body camber and body indentation on longitudinal characteristics of 60° deltawing-body combination at Mach number of 1,61 [with list of references]; by John R. Sevier, jr..

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Apr. 20, 1956
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

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