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Author: Harry E. Murray
Publisher:
Published: 1950
Total Pages: 744
ISBN-13:
DOWNLOAD EBOOKThe lateral motions of aircraft are obtained by means of the Laplace transform which gives solutions in terms of elementary functions for the free motions and the motions due to forcing step functions. The lateral stability of a specific airplane and certain of its free and forced motions are calculated.
Author: United States. National Advisory Committee for Aeronautics
Publisher:
Published: 1952
Total Pages: 32
ISBN-13:
DOWNLOAD EBOOKAuthor:
Publisher:
Published: 1973
Total Pages: 528
ISBN-13:
DOWNLOAD EBOOKAuthor: United States. National Advisory Committee for Aeronautics
Publisher:
Published: 1951
Total Pages: 654
ISBN-13:
DOWNLOAD EBOOKAuthor: Richard R. Heldenfels
Publisher:
Published: 1950
Total Pages: 712
ISBN-13:
DOWNLOAD EBOOKA method is presented for the approximate calculation of the stresses and distortions in a box beam representing the main structural component of a swept wing with a carry-through section and with bulkheads perpendicular to the spars. The application of the method is illustrated by a numerical example and its results are compared with previously published test data.
Author: A. A. Kirsch
Publisher:
Published: 1954
Total Pages: 108
ISBN-13:
DOWNLOAD EBOOKAuthor: J. F. McCarthy (Jr)
Publisher:
Published: 1953
Total Pages: 90
ISBN-13:
DOWNLOAD EBOOKAuthor: United States. National Advisory Committee for Aeronautics
Publisher:
Published: 1954
Total Pages: 1200
ISBN-13:
DOWNLOAD EBOOKIncludes the Committee's Technical reports no. 1-1058, reprinted in v. 1-37.
Author: United States. National Advisory Committee for Aeronautics
Publisher:
Published: 1950
Total Pages: 996
ISBN-13:
DOWNLOAD EBOOKAuthor: Antonio Ferri
Publisher:
Published: 1951
Total Pages: 328
ISBN-13:
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