Publisher: National Aeronautics and Space Administration / Publish Year Decade: 1960 - 1969 - Blacklight Search Results

Start Over Publisher National Aeronautics and Space Administration Publish Year Decade 1960 - 1969

9391. NACA research memorandum RM (series). E55C01. Investigation of boattail and base pressures of twin-jet afterbodies at Mach number 1.91 [with list of references]; by Reino J. Salmi and John L. Klann. Washington, Apr. 21, 1955

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: [January 1961]
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

9392. NACA research memorandum RM (series). E55D15. Experimental investigation of direct control of diffuser pressure on 16-inch ram-jet engine [with list of references]: by William R. Dunbar, George Vasu, and Herbert G. Hurrell. Washington, June 20, 1955.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: [January 1961]
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

9393. NACA research memorandum RM (series). E56A17. Performance of supersonic ramp-type side inlet with combinations of fuselage and inlet throat boundary-layer removal [with list of references]; by Robert C. Campbell. Washington, Apr. 25, 1956

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: [January 1961]
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

9394. NACA research memorandum RM (series). E56A30. Factors controlling air-inlet flow distortions; by William H. Sterbentz. Washington, Apr. 6, 1956

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: [January 1961]
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

9395. NACA research memorandum RM (series). E56C07. Experimental and analytical investigation of acceleration regulating control for turbojet engine [with list of references]; by Paul M. Stiglic, Herbert Heppler, and David Novik. Washington, June 28, 1956.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: [January 1961]
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

9396. NACA research memorandum RM (series). L55H22b. Initial experimental investigation of aerodynamic load on wing of model caused by blast-induced gust that increases angle of attack into stall region [with list of references]: by Harold B. Pierce and Thomas D. Reisert. Washington, Dec. 19, 1955

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: [January 1961]
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

9397. NACA research memorandum RM (series). L56C14. Effect of leading-edge droop on aerodynamic and loading characteristics of 4-percent-thick unswept-wing-fuselage combination at transonic speeds [with list of references]: by James W. Schmeer. Washington, May 23, 1956.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: [January 1961]
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

9398. NACA research memorandum RM (series). L56D17. Force and pressure-distribution measurements at Mach no. 3.12 of slender bodies having circular, elliptical, and triangular cross sections and same longitudinal distribution of cross-sectional area [with list of references]: by Roy H. Lange and Charles E. Wittliff. Washington, July 13, 1956.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: [January 1961]
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

9399. NACA research memorandum RM (series). L56L19. Longitudinal and lateral stability and control characteristics of 2 canard airplane configurations at Mach numbers of 1.41 and 2.01 [with list of references]: by Cornelius Driver. Washington, Apr. 10, 1957

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: [January 1961]
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

9400. NACA research memorandum RM (series). L57A24. Experimental investigation of effects of Mach number, stabilizer dihedral, and fin torsional stiffness on transonic flutter characteristics of tee-tail [with list of references]; by Norman S. Land and Annie G. Fox. Washington, Oct. 23, 1957

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: [January 1961]
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

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