NASA-TM-X-213
Investigation of the aerodynamic characteristics of a supersonic horizontal- attitude VTOL airplane model at Mach numbers of 1.57, 2.14, 2.54, and 2.87
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Abstract:
Drag and static longitudinal and lateral stability characteristics of supersonic horizontal attitude VTOL aircraft model in wind tunnel
Author(s):
A.E. Franklin; R.M. Lust
Indexed under:
- None
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