Stability and control characteristics of a monoplanar missile configuration with two low-profile tail arrangements at Mach numbers from 1.70 to 2.86 /
An experimental wind tunnel investigation has been made to determine the longitudinal and lateral aerodynamic stability and control characteristics of two tail fin arrangements of a monowing missile model. Both a conventional cruciform and a low profile tail arrangement were tested. The results indi...
|Format:||Government Document Book|
Washington : Springfield, Va. :
National Aeronautics and Space Administration ; For sale by the National Technical Information Service,
|Series:||NASA technical note ;
NASA TM X-3533. |