Annual Report of the National Advisory Committee for Aeronautics, Issues 834-862

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Includes the Committee's Technical reports no. 1-1058, reprinted in v. 1-37.
 

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Page 1 - In the event of a laboratory or laboratories, either in whole or in part, being placed under the direction of the committee, the committee may direct and conduct research and experiment in aeronautics in such laboratory or laboratories...
Page 72 - Q are related by р/с' = constant, where y is the ratio of specific heat at constant pressure to specific heat at constant volume, for compressible fluids.
Page 41 - Standards; together with not more than five additional persons who shall be acquainted with the needs of aeronautical science, either civil or military, or skilled in aeronautical engineering or its allied sciences...
Page 1 - ... transportation expense, equals or exceeds 55 percent of the current GSA Stores Stock Catalog price, the Federal Supply Schedule price, or current market price of new items of the same type and class. (b) The 55 percent criterion prescribed in § 101-25.404(a) (2) is the minimum standard and may be exceeded when it is to the advantage of the Government to do so. Executive agencies may rehabilitate items of furniture subject to replacement under the standard when the rehabilitation improves the...
Page 320 - It is possible that this autoignition may set up detonation [a detonation wave] in some cases, thereby acting as an intermediate stage in knocking. Our experiments have not been carried to a definite conclusion, and present data do not warrant presentation of autoignition as a positive explanation for knocking. It is our feeling, however, that information at hand favors more strongly the theory of autoignition of the high-density gases ahead of the flame front than that of detonation [the detonation...
Page 41 - NATIONAL ADVISORY COMMITTEE FOR AERONAUTICS The National Advisory Committee for Aeronautics was established by act of Congress approved March 3, 1915, and the membership increased from 12 to 15 by act approved March 2, 1929 (USC, title 50, sec.
Page 121 - LANGLEY MEMORIAL AERONAUTICAL LABORATORY, NATIONAL ADVISORY COMMITTEE FOR AERONAUTICS, LANGLEY FIELD, VA., April 29, 1946.
Page 95 - Lateral Stability Characteristics, II — Rectangular Midwing on Circular Fuselage with Variations in Vertical-Tail Area and Fuselage Length with and without Horizontal Tail Surface,
Page 1 - supervise and direct the scientific study of the problems of flight with a view to their practical solution.

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