Stability Analysis of Plates and Shells PDF Download
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Author:
Publisher:
ISBN:
Category : Plates (Engineering)
Languages : en
Pages : 460
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Book Description
Author:
Publisher:
ISBN:
Category : Plates (Engineering)
Languages : en
Pages : 460
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Book Description
Author: Antonio Ferri
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 232
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Book Description
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 836
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Book Description
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 730
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Book Description
Author: Ralph W. Stone (Jr.)
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 560
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Book Description
An investigation was made in the Langley 15-foot free-spinning tunnel to determine the effect of horizontal-tail position on rudder hinge-moments at attitudes simulating spinning conditions. Hinge-moment measurements were made on an unbalanced rudder on a rectangular vertical tail for six positions of the horizontail tail. The hinge-moment measurements were supplemented by tuft tests to determine the air flow about the vertical tail.
Author: William R. Campbell
Publisher:
ISBN:
Category : Strain gages
Languages : en
Pages : 690
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Book Description
Tests were made to determine the important performance characteristics for six types of bakelite-bonded wire strain gages commercially available and in current use by the aircraft industry. Results on the following characteristics are presented: (1) uniformity of calibration factors for individual gages of the same type, (2) variation of calibration factor with temperature, (3) creep, (4) effect of current on gage resistance, and (5) variation of gage resistance with temperature.
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 548
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Book Description
Author: A. V. Viswanathan
Publisher:
ISBN:
Category : Buckling (Mechanics)
Languages : en
Pages : 76
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Book Description
Author: Arthur M. Trout
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 608
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Book Description
Charts are presented by means of which the jet pressure ratio that give optimum division of power between propeller and jet for maximum total thrust power may be determined for any turbine-propeller engine with or without intercooling, reheat, regeneration, or any combination of these modifications.
Author: S. B. Batdorf
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 38
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Book Description
Summary: An exact solution and a closely concurring approximate energy solution are given for the buckling of an infinitely long flat plate under combined shear and transverse direct stress with edges elastically restrained against rotation. It was found that an appreciable fraction of the critical stress in pure shear may be applied to the plate without any reduction in the transverse compressive stress necessary to produce buckling. An interaction formula in general use was shown to be decidedly conservative for the range in which it is supposed to apply.
