Author: National Aeronautics and Space Administration / Publisher: National Aeronautics and Space Administration - Blacklight Search Results

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16551. NACA research memorandum RM (series). L57C18. Heat-transfer and pressure distribution on 6 blunt noses at Mach number of 2 [with list of references]; by Howard S. Carter and Walter E. Bressette.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Apr. 18, 1957
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

16552. NACA research memorandum RM (series). L57D04a. Measurements of heat transfer and boundary-layer transition on 8-inch-diameter hemisphere-cylinder in free flight for Mach number range of 2.00 to 3.88 [with list of references]; by Benjamine J. Garland and Leo T. Chauvin.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Apr. 18, 1957
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

16553. NACA research memorandum RM (series). L57D05. Heat transfer and boundary-layer transition on highly polished hemisphere-cone in free flight at Mach numbers up to 3.14 and Reynolds numbers up to 24 × 10° [with list of references]; by James J. Buglia.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Apr. 18, 1957
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

16554. NACA research memorandum RM (series). E57B05. Interrelated effects of engine rotor momentum and flight regime on dynamic stability of high-performance aircraft [with list of references]; by Warren J. North.

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

16555. NACA research memorandum RM (series). L57A29. Transonic investigation of internal-flow characteristics of square-shaped scoop inlet mounted at 3 chordwise positions above high 45° sweptback wing and body combination [with list of references]; by Arvid L. Keith, jr.

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

16556. NACA research memorandum RM (series). L57C08. Experimental study at high subsonic speeds of several tall configurations on model having 45° sweptback wing [with list of references]: by William C. Sleeman, jr..

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

16557. NACA research memorandum RM (series). L56K23. Investigation of high-performance axial-flow compressor transonic Inlet rotor designed for 37.5 pounds per second per square foot of frontal area, detailed blade-element performance [with list of references]; by A. Richard Felts and Melvyn Savage.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Apr. 12, 1957
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

16558. NACA research memorandum RM (series). L57B01. Hinge-moment characteristics for series of controls and balancing devices on 60° delta wing at Mach numbers of 1.61 and 2.01 [with list of references]; by Douglas R. Lord and K. R. Czarnecki.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Apr. 12, 1957
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

16559. NACA research memorandum RM (series). L57B21. Jet effects on drag of conical afterbodies for Mach numbers of 0.6 to 1.28 [with list of references]; by James M. Cubbage, jr.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Apr. 12, 1957
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

16560. NACA research memorandum RM (series). L57B07. Transonic investigation of mass-flow and pressure recovery characteristics of several types of auxiliary air inlets [with list of references]; by John S. Dennard.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Apr. 10, 1957
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

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