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
01.08.1975
Report
Keine Angabe
Englisch
Correlation of wind-tunnel and flight-test stability and control data for SB2C-1 airplane
Engineering Index Backfile | 1948
|