Wind tunnel/flight data correlation for the Boeing 737-100 transport airplane
F. J. Capone
Abstract
Open-access reader
F. J. Capone
Abstract
Open-access reader
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.
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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.
Key concepts: Airplane, Wind tunnel, Mach number, Drag, Meteorology, Aerospace engineering, Lift (data mining), Lift-to-drag ratio