Publication Date:
2011-08-18
Description:
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).
Keywords:
AERODYNAMICS
Type:
Wind-Tunnel(Flight Correlation, 1981; p 65-91
Format:
text
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