Rocket-model investigation of lateral stability characteristics and power effects of a jet-engine airplane configuration with tail boom at mach numbers from 1.15 to 1.37 /
by T. Bradley, Jr., and Normal L. Crabill.
Description
- Language(s)
-
English
- Published
-
Washington, D.C. : National Aeronautics and Space Administration : [1961]
- Note
-
Cover title.
"January 1961."
Aerodynamics, aircraft; Stability and control.
- Physical Description
-
29 p. :
ill. ;
26 cm.
Viewability
Item Link |
Original Source |
Full view v.638
|
University of Illinois at Urbana-Champaign
|