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

991. NACA research memorandum RM (series). L54I10. Low-amplitude damping-in-pitch characteristics of 4 tailless swept wing-body combinations at Mach numbers from 0.85 to 1.30 as obtained with rocket-powered models [with list of references]; by Charles T. D'Aiutolo

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Nov. 24, 1954
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

992. NACA research memorandum RM (series). A54H23a. Investigation of lift, center of pressure, and drag of projectile at Mach number of 8.6 and Reynolds number of 17 million [with list of references]; by Thomas N. Canning.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Nov. 19, 1954
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

993. NACA research memorandum RM (series). L54107a. Experimental transonic investigation of 45° sweptback wing-body combination with several types of body indentation with theoretical comparisons included [with list of references]; by Melvin M. Carmel.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Nov. 19, 1954
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

994. NACA research memorandum RM (series). E54G23a. Analysis and construction of design charts for turbines with downstream stators [with list of references]; by Richard H. Cavicchi and Anita B. Constantine.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Nov. 18, 1954
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

995. NACA research memorandum KM (series). E54I14. Effectiveness of boundary-layer removal near throat of ramp-type side inlet at free-stream Mach number 2.0 [with list of references]; by Leonard J. Obery and Kobert W. Cubbison.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Nov. 17, 1954
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

996. NACA research memorandum RM (series). E54G22. Altitude-wind-tunnel investigation of several afterburner configurations having moderately high burner-inlet velocities [with list of references]: by F. W. Schulze, H. E. Bloomer, and R. R. Miller.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Nov. 17, 1954
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

997. NACA research memorandum RM (series). E54H19. Thrust and pumping characteristics of series of ejector-type exhaust nozzles at subsonic and supersonic flight speeds [with list of references]; by Donald P. Hearth and Alfred S. Valerino.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Nov. 17, 1954
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

998. NACA research memorandum RM (series). E54I01. Performance of supersonic ramp inlet with internal boundary-layer scoop [with list of references]; by Robert C. Campbell.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Nov. 17, 1954
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

999. NACA research memorandum RM (series). A54D05. Wind-tanned investigation at subsonic and supersonic speeds of fighter model employing low-aspect-ratio unswept wing and horizontal tail mounted well above wing plane, longitudinal stability and control [with list of references]; by Willard G. Smith.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Nov. 15, 1954
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

1000. NACA research memorandum RM (series). L54I01. Longitudinal stability characteristics at transonic speeds of canard configuration having 45° sweptback wing of aspect ratio 6.0 and NACA 65A009 airfoil section [with list of references]; by A. James Vitale and John C. McFall, jr.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Nov. 15, 1954
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

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