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211. Technical notes. 4405. Free-flight investigation to determine drag of flatand vee-windshield canopies on parabolic fuselage with and without transonic indentation between Mach numbers of 0.75 and 1.35 [with list of references]; by Walter L. Kouyoumjian and Sherwood Hoffman.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Sept. 1958
SuDoc number:: Y 3.N 21/5:6/(nos.)

212. Technical notes. 4406. Low tire friction and cornering forces on wet surface [with list of references]; by Eziaslav N. Harrin.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Sept. 1958
SuDoc number:: Y 3.N 21/5:6/(nos.)

213. Technical notes. 4407. Effects of ground proximity on thrust of simple downward-directed jet beneath flat surface [with list of references]; by Kenneth P. Spreemann and Irving R. Sherman.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Sept. 1958
SuDoc number:: Y 3.N 21/5:6/(nos.)

214. Technical notes. 4408. Theory of diffusion in strained systems [with list of references]; by Louis A. Girifalco and Hubert H. Grimes.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Sept. 1958
SuDoc number:: Y 3.N 21/5:6/(nos.)

215. Technical notes. 4409. Flight measurements of vibration experienced by tandem helicopter in transition, vortex-ring state, landing approach, and yawed flight [with list of references]; by John E. Yeates.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Sept. 1958
SuDoc number:: Y 3.N 21/5:6/(nos.)

216. Technical notes. 4410. Flight measurements of vibratory stresses on propeller designed for advance ratio of 4.0 and a Mach number of 0.82 [with list of references]; by Thomas C. O'Bryan.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Sept. 1958
SuDoc number:: Y 3.N 21/5:6/(nos.)

217. NACA research memorandum RM (series). A58E19. Experimental investigation of effect of yaw on rates of heat transfer to transverse circular cylinders in 6500-foot-per-second hypersonic air stream [with list of references]: by Bernard E. Cunningham and Samuel Kraus.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Aug. 26, 1958
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

218. NACA research memorandum RM (series). A58E21n. Forces and pitching moments on aspect-ratio-3.1 wing-body combination at Mach numbers from 2.5 to 3.5 and sublimation studies of effect of single-element roughness on boundary-layer flow [with list of references]; by Edward J. Hopkins, Stephen J. Keating, jr., and Richard R. Muhl.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Washington, Aug. 26, 1958
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

219. NACA research memorandum RM (series). L58F26. Investigation of tilting-wing vertical-take-off-and-landing jet airplane model in hovering and transition flight [with list of references]; by Robert H. Kirby and James L. Hassell, jr.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Aug. 26, 1958
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

220. Research memorandum RM (series). L58C28a. Landing and taxiing tests over various types of runway lights [with list of references]; by Robert C. Dreher and Sidney A. Batterson.

Corporate/Agency Authors:: National Advisory Committee for Aeronautics
Publisher:: National Advisory Committee for Aeronautics
Date:: Aug. 26, 1958
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

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