Buckling of aerodynamic surfaces may have adverse effect on aircraft performance; temperature distributions for which buckling occurs should be known; it may not be feasible to design structure which will not buckle and for these cases magnitude of distortions should be known in order that their effect on aircraft performance may be estimated; approximate method given.
Thermal buckling of plates
NACA -- Tech Note
1952
39 pages
Report
English
© Metadata Copyright Elsevier B. V. All rights reserved.
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