The XB-70-1 was selected for a wind-tunnel/flight correlation program as representative of a large, flexible supersonic airplane similar to a supersonic transport. Tests were made to determine the effects of control deflections, wing tip deflection, and variations in inlet mass flow (additive drag).
Wind-tunnel/flight correlation program on XB-70-1
1982-06-01
Conference paper
No indication
English
Wind-tunnel/flight-drag correlation
NTRS | 1982
|Wind-Tunnel/Flight Correlation, 1981
NTRS | 1982
|Wind-Tunnel/ Flight Correlation: 1981 : Proceedings
TIBKAT | 1982
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