Free Flight Investigation At Mach Numbers Between 0 5 And 1 7 Of The Zero Lift Rolling Effectiveness And Drag Of Various Surface Spoiler And Jet Controls On An 80 Delta Wing Missile
Download Free Flight Investigation At Mach Numbers Between 0 5 And 1 7 Of The Zero Lift Rolling Effectiveness And Drag Of Various Surface Spoiler And Jet Controls On An 80 Delta Wing Missile PDF/ePub or read online books in Mobi eBooks. Click Download or Read Online button to get Free Flight Investigation At Mach Numbers Between 0 5 And 1 7 Of The Zero Lift Rolling Effectiveness And Drag Of Various Surface Spoiler And Jet Controls On An 80 Delta Wing Missile book now. This website allows unlimited access to, at the time of writing, more than 1.5 million titles, including hundreds of thousands of titles in various foreign languages.
Index of NASA Technical Publications
Author: United States. National Aeronautics and Space Administration
language: en
Publisher:
Release Date: 1959