28 cm, 72, wraps, illus., figures, charts, references, covers worn, text separated from covers Contains articles on theorems concerning the drag reduction of wings of fixed plan form, temperature distribution and thermal stresses in a model of a supersonic wing, a general method for solving problems of the unsteady lifting surface theory in the subsonic range, single degree of freedom flutter of compressor blades in separated flow, temperature distribution in laminar stagnation-point flow with axisymmetry, limit design of columns, and design and performance of an adjustable two-dimensional nozzle with boundary-layer correction.

N� de ref. del art�culo 45582

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Detalles bibliogr�ficos

T�tulo

Journal of the Aeronautical Sciences, Volume 21, Number 1, January 1954

Editor

Inst/Aeronautical Sciences, Easton, PA

Fecha de publicaci�n

1954

Estado

fair

Cat�logos de vendedores

Aircraft

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