Publication Date:
2019-08-17
Description:
At the request of the Henschel Aircraft Works. A. G. Berlin. three models of the missile "Zitterrochen" were investigated at subsonic velocities.(open jet 215-millimeter diameter) and at supersonic velocities (open jet 110 by 130 millimeters) in order to determine the effect of various wing forms on the air forces and moments. Three-component measurements were taken, and one model was also investigated with deflected control plates.
Keywords:
Aircraft Stability and Control
Type:
NACA-TM-1159
,
DLUM-3122
,
Deutsche Luftfahrtforschung, Untersuchungen und Mitteilungen
Format:
application/pdf