Search the Libraries' digital collections -- images, media, maps, and more...

A Preliminary Investigation to Study the Effect of Flat Spoilers on the Aerodynamic Characteristics of Wings at Angles of Attack from 0 Deg to 90 Deg

Dome Repository

Files in this item

DTMB_1966_2214.pdf 5.272Mb PDF

This item appears in the following Collection(s)

Search Dome