Spanwise loading for wings and control surfaces of low aspect ratio
John Deyoung
Abstract
Open-access reader
John Deyoung
Abstract
Open-access reader
From considerations of the linearized-compressible-flowequation, the aero@namic values given by zero-as~ct-ratio theory are also those of moderat=spect+atio wings at the speed applicable for low values of the product of pressibility parameter and aspect ratio.
OpenAlex reports 10 citations for this work. Citation counts describe recorded attention and do not establish research quality.
A contribution statement is not available in the OpenAlex record.
Method details are not available in the OpenAlex metadata.
Findings are not separately available in the OpenAlex metadata.
Limitations are not available in the OpenAlex metadata.
Application details are not available in the OpenAlex metadata.
From considerations of the linearized-compressible-flowequation, the aero@namic values given by zero-as~ct-ratio theory are also those of moderat=spect+atio wings at the speed applicable for low values of the product of pressibility parameter and aspect ratio.
Key concepts: Aspect ratio (aeronautics), Materials science, Composite material