A brief wind-tunnel/flight data correlation for the Boeing 737-100 airplane was made. The results showed excellent agreement between wind-tunnel and flight trimmed drag polars at Mach numbers less than 0.67. The wind-tunnel data predicted larger drag increments due to compressibility and a lift-curve slope about 9 percent higher than flight.
Wind tunnel/flight data correlation for the Boeing 737-100 transport airplane
1975-08-01
Report
No indication
English
Flight Control System for The Boeing 2707 Supersonic Transport Airplane
SAE Technical Papers | 1967
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