An analysis of the fatigue life of an airplane wing structure under overload conditions / by Abbott A. Putnam and Thomas D. Reisert.

Saved in:
Bibliographic Details
Main Author: Putnam, Abbott A.
Corporate Authors: United States. National Advisory Committee for Aeronautics, Langley Aeronautical Laboratory
Other Authors: Reisert, Thomas D.
Other title:NACA Wartime Reports. Series L.
Format: Government Document Book
Language:English
Published: Washington, D.C. : National Advisory Committee for Aeronautics, [1946]
Series:Wartime Reports (United States. National Advisory Committee for Aeronautics) ; no. L10.
Subjects:
Search Result 1

Aerodynamic characteristics of four NACA airfoil sections designed for helicopter rotor blades / by Stivers, Louis S.

Published 1946
Government Document Book
Search Result 2
Search Result 3

Aerodynamic data for a wing section of the Republic XF-12 airplane equipped with a double slotted flap / by Cahill, Jones F.

Published 1946
Government Document Book
Search Result 4
Search Result 5

An analysis of the indications of the University of Chicago airborne turbulence indicator in gusty air / by Tolefson, H. B.

Published 1946
Government Document Book
Search Result 6

Analysis of V-G records from the SNB-1 airplane / by Walker, Walter G.

Published 1946
Government Document Book
Search Result 7
Search Result 8

Calibrations of service pitot tubes in the Langley 24-inch high-speed tunnel / by Lindsey, W. F.

Published 1946
Government Document Book
Search Result 9

Charts for critical combinations of longitudinal and transverse direct stress for flat rectangular plates / by Libove, Charles

Published 1946
Government Document Book
Search Result 10
Search Result 12
Search Result 13

A correlation of loadings and afterbody length-beam ratios of various flying-boat hulls / by Parkinson, John B.

Published 1946
Government Document Book
Search Result 14

Correlation tests of the ditching behavior of an Army B-24D airplane and a 1/16-size model / by Jarvis, George A.

Published 1946
Government Document Book
Search Result 16

Determination of induced velocity in front of an inclined propeller by a magnetic-analogy method / by Gardner, Clifford S.

Published 1946
Government Document Book
Search Result 18

Determination of towline tension and stability of spin-recovery parachutes / by Wood, John H.

Published 1946
Government Document Book
Search Result 19

Development of wing inlets / by Racisz, Stanley F.

Published 1946
Government Document Book
Search Result 20