Thermal effects on static aeroelastic stability and control.


Autoria(s): Bell Aircraft Corporation.
Data(s)

28/09/2024

Resumo

v. 1. Methods of predicting structural temperatures due to aerodynamic heating, by A. H. Blessing.--v. 2. Aerodynamics, by J. R Batt.--v. 3. Experimental and analytical methods for the determination of thermally-affected wing deflectional behavior, by R. H. Gallagher.--v. 3. sup. Description and results of tests conducted to determine the thermally affected behavior of corrugated multiweb wing structures, by J. F. Quinn.

Mode of access: Internet.

Formato

bib

Identificador

http://hdl.handle.net/2027/coo.31924004633511

Idioma(s)

eng

Publicador

Wright-Patterson Air Force Base, Ohio, Wright Air Development Center, Air Research and Development Command, U. S. Air Force,

Direitos

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Palavras-Chave #Aerodynamic heating #Aerodynamics #Aeroelasticity
Tipo

text