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

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16971. NACA research memorandum RM (series). L55D13. Experimental investigation of zero-lift wave drag of 7 pairs of delta wings with constant and varying thickness ratios at Mach numbers of 1.62, 1.93, and 2.41 [with list of references]; by Arthur Henderson, jr..

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

16972. NACA research memorandum RM (series). E55A31. Analytic evaluation of effect of inlet-air temperature and combustion pressure on combustion performance of boron slurries and blends of pentaborane in octene-1 [with list of references]; by Leonard K. Tower.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: June 1, 1955
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

16973. NACA research memorandum RM (series). E55B28. Investigation of high-pressure-ratio 8-stage axial-flow research compressor with 2 transonic inlet stages: 4, Modification of aerodynamic design and prediction of performance [with list of references]; by Richard P. Geye and Charles H. Voit.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: June 1, 1955
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

16974. NACA research memorandum RM (series). E55C07. Experimental evaluation of boron-hydrocarbon slurry in 10-inch ramjet combustor [with list of references]; by William R. Kerslake, E. E. Dangle, and A. J. Cervenka.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: June 1, 1955
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

16975. NACA research memorandum RM (series). A55C30a. Effect of wing fences on longitudinal characteristics at Mach numbers up to 0.92 of wing-fuselage-tail combination having 40° swept-back wing with NACA 64A thickness distribution [with list of references]; by Jerald K. Dickson and Fred B. Sutton.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: May 27, 1955
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

16976. NACA research memorandum RM (series). A55D08. Experimental investigation of some aerodynamic effects of gap between wing and body of moderately slender wing-body combination at Mach number of 1.4 [with list of references]; by Duane W. Dugan.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: May 27, 1955
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

16977. NACA research memorandum RM (series). A55D12. Controls for supersonic missiles [with list of references]; by George E. Kaattari, William A. Hill, jr., and Jack N. Nielsen.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: May 27, 1955
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

16978. NACA research memorandum RM (series). A55D12a. Effects of powered controls and fire-control systems on tracking accuracy [with list of references]; by George A. Rathert, jr., Marvin Abramovitz, and Burnett L. Gadeberg.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: May 26, 1955
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

16979. NACA research memorandum RM (series). L54120. Experimental Investigation at high subsonic speeds of rolling stability derivatives of complete model with aspect-ratio-2.52 wing having unswept 72-percent-chord line and high horizontal tall [with list of references]; by William C. Sleeman, jr., and James W. Wiggins.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: May 26, 1955
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

16980. NACA research memorandum RM (series). L54G08. Static longitudinal and lateral stability and control characteristics of model of 35° swept-wing airplane at Mach number of 1.41 [with one reference]; by Edward B. Polazzo and M. Leroy Spearman.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: May 26, 1955
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

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