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. (Author)
Wind Tunnel/Flight Data Correlation for the Boeing 737-100 Transport Airplane
1975
18 pages
Report
Keine Angabe
Englisch
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