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

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

10121. NACA research memorandum RM (series). L57L13. Tests of aerodynamically heated multiweb wing structures in free jet at Mach number 2: 4 aluminum-alloy models of 20-inoh chord and span with 0.004-inch-thick skin, 0.025-inch-thick ribs and webs, and zero, 1, 2, or 3 chordwise ribs [with list of references]: by John R. Davidson, Richard Rosecrans, and Louis F. Vosteen.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: May 8, 1958
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

10122. NACA research memorandum RM (series). L58B18. Heat transfer for Mach numbers up to 2.2 and pressure distributions for Mach numbers up to 4.7 from flight investigations of flat-facecone and hemisphere-cone I with list of references]; by Katherine C. Speegle, Leo T. Chauvin, and Jack C. Heberlig.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: May 8, 1958
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

10123. NACA research memorandum RM (series). E57H28. Experimental results of investigation of 2 methods of inflight thrust measurement applicable to afterburning turbojet engines with ejectors [with list of references]; by Harry E. Bloomer.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: May 2, 1958
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

10124. NACA research memorandum RM (series). L58B25. Effect of control trailing-edge thickness or aspect ratio on oscillating hinge-moment and flutter characteristics of flap-type control at transonic speeds [with list of references]; by William C. Moseley, jr., and Robert F. Thompson.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Apr. 23, 1958
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

10125. NACA research memorandum RM (series). A57K07. Analytical evaluation of effects of aerodynamic modification and of stability augmenters on pitch-up behavior and probable pilot opinion of 2 current fighter airplanes [with list of references); by Melvin Sadoff and John D. Stewart.

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

10126. NACA research memorandum RM (series). H58A30. Analysis of surface pressures and aerodynamic load distribution over swept wing of Douglas D-558-II research airplane at Mach numbers from 0.73 to 1.73 [with list of references]; by Norman V. Taillon.

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

10127. NACA research memorandum RM (series). L58B04. Free-flight investigation to determine inlet external drag of 4 inlet models at Mach numbers from 1.50 to 3.00 [with list of references]; by Walter L. Kouyoumjian.

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

10128. NACA research memorandum RM (series). L58A31. Effects of shock-boundary-layer interaction on performance of long and short subsonic annular diffuser [with list of references]; by Charles C. Wood and John R. Henry.

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

10129. NACA research memorandum RM (series). A58A14. Wind-tunnel data on longitudinal and lateral-directional rotary derivatives of straight-wing, research airplane configuration at Mach numbers from 2.5 to 8.5 [with list of references]; by Benjamin H. Beam and Kenneth C. Endicott.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Mar. 25, 1958
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

10130. NACA research memorandum RM (series). L57K22. Feasibility of nose-cone cooling by upstream ejection of solid coolants at stagnation point [with list of references]; by William H. Kinard.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Mar. 24, 1958
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

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