English (United Kingdom)

https://curated-unify.zendy.io/wp-json/zendy-region/v1/featured_content/oa?rat=en

https://curated-unify.zendy.io/wp-json/zendy-region/v1/highlighted_journal/

Zendy Plus

Presents the access of premium content as premium feature

Premium Content

Presents the keyphrase highlighting as premium feature

Keyphrase Highlighting

Presents the summarisation as premium feature

Summarisation

Insights

Presents the pdf analysis as premium feature

PDF Analysis

Presents the zaia usage as premium feature

ZAIA

Zendy Tools

Zendy Open

The deformations of the wing-sections and the stressed-skins of a high speed airplane will give a great effect on it's aerodynamic performance. In this second report based on the first report [1] already published, the deflection of a skin panel subjected to flight and thermal loads is analysed, and the equation with which the skin thickness needed to fulfil the requirements of allowance for the variations of a wing section can be calculated is presented. As one of the results, it is found that the aerodynamic requirements such that the forms of wing sections should be kept accurately within some allowance of deformation might often become considerably severe in the design of skin panel and the effect of elastic deformations should carefully be considered.

On the Effect of Flight Loads and Aerodynamic Heating on the Deformations of Stressed Skins, especially of Wing Sections of High Speed Airplanes