Gottingen Wind Tunnel for testing aircraft models

Book details

Title
Gottingen Wind Tunnel for testing aircraft models
Publication year listed
1920
Format
Public domain eBook
Reading access
Free online reader; no registration required
Source record
View on Archive.org

About this book

Gottingen Wind Tunnel for testing aircraft models

Author: Prandtl,

Year: 1920

Given here is a brief description of the Gottingen Wind Tunnel for the testing of aircraft models, preceded by a history of its development. Included are a number of diagrams illustrating, among other things, a sectional elevation of the wind tunnel, the pressure regulator, the entrance cone and method of supporting a model for simple drag tests, a three-component balance, and a propeller testing device, all of which are discussed in the text.

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