Wind tunnel pressure distribution tests on a series of biplane wing models

Book details

Title
Wind tunnel pressure distribution tests on a series of biplane wing models
Publication year listed
1929
Format
Public domain eBook
Reading access
Free online reader; no registration required
Source record
View on Archive.org

About this book

Wind tunnel pressure distribution tests on a series of biplane wing models

Author: Knight, Montgomery

Year: 1929

This report is on the changes in forces on each wing of a biplane cellule when either the stagger or the gap is varied. Since each test was carried up to a 90 degree angle of attack, the results may be used in the study of stalled flight and of spinning as well as in the structural design of biplane wings.

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