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

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16881. NACA research memorandum RM (series). L55I13. Flight investigation of effect of underwing propulsive jets on lift, drag, and longitudinal stability of delta-wing configuration at Mach numbers from 1.23 to 1.62 [with list of references]; by Ralph A. Falanga and Joseph H. Judd.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Dec. 15, 1955
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

16882. NACA research memorandum RM (series). L55I27a. Origin and distribution of supersonic store interference from measurement of individual forces on several wing-fuselage-store configurations: 4, Delta-wing heavy-bomber configuration with large store, Mach number, 1.61 [with list of references]; by Odell A. Morris.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Dec. 15, 1955
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

16883. NACA research memorandums RM (series). E55I14. Performance of single fuel-vaporizing combustor with 6 injectors adapted for gaseous hydrogen [with list of references]; by Jerrold D. Wear and Arthur L. Smith.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Nov. 30, 1955
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

16884. NACA research memorandum RM (series). A55H04a. Effect of leading-edge sweepback on lift, drag, and pitching-moment characteristics of thin wings of aspect ratio 3 and taper ratio 0.4 at subsonic and supersonic speeds [with list of references]; by Benton E. Wetzel.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Nov. 18, 1955
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

16885. NACA research memorandum RM (series). E55F20. Effect of inlet flow distortion on compressor stall and acceleration characteristics of J65-B-3 turbojet engine [with list of references]; by David B. Fenn and Joseph N. Sivo.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Nov. 18, 1955
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

16886. NACA research memorandum RM (series). E55H03. Experimental investigation of surge control on turbojet engine [with list of references]; by David Novik, Herbert Heppler, and Paul M. Stiglic.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Nov. 18, 1955
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

16887. NACA research memorandum RM (series). E55H16a. Effect of centerbody boundary-layer removal near throat of 3 conical nose inlets at Mach 1.6 to 2.0 [with list of references]; by Emil J. Kremzier and George A. Wise.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Nov. 15, 1955
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

16888. NACA research memorandum RM (series). E55H25a. Throat-area determination for cascade of double-circular-arc blades [with list of references]; by Linwood C. Wright and Richard Schwind.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Nov. 15, 1955
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

16889. NACA research memorandum RM (series). L55H12. Aerodynamic loads on external store adjacent to 45° sweptback wing at Mach numbers from 0.70 to 1.96, including evaluation of techniques used [with list of references]; by Lawrence D. Guy and William M. Hadaway.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Nov. 15, 1955
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

16890. NACA research memorandum RM (series). L55I26. Lateral-control investigation at transonic speeds of differentially deflected horizontal-tail surfaces for configuration having 6-percent-thick 45° sweptback wing [with] list of references]; by Chris C. Critzos.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Nov. 15, 1955
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

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