From inside the book

What people are saying - Write a review

We haven't found any reviews in the usual places.

Other editions - View all

Common terms and phrases

Popular passages

Page 22 - Glauert, H.: The Effect of the Static Pressure Gradient on the Drag of a Body Tested in a Wind Tunnel.
Page 3 - drag. The boundaries had no appreciable effect on the pitching moments of either the airfoils or the complete airplane model. Increasing turbulence appeared to increase the minimum drag and maximum lift and to decrease the pitching moment.
Page 22 - Wieselsberger, C.: Wind Tunnel Tests of Correction Formula for wings of Large Span.
Page 3 - the purpose of obtaining a method of correcting to free air conditions the results of airfoil force tests in
Page 4 - in the Atmospheric Wind Tunnel of the Langley Memorial Aeronautical Laboratory, the

Bibliographic information