The purpose of the report is to predict drag increment due to rear fuselage upsweep. The results may be applied to the calculation of cruise drag. The research is relevant to military and civil transport aircraft, subcritical Mach numbers.
Drag Increment Due to Rear Fuselage Upsweep
1980
10 pages
Report
Keine Angabe
Englisch
Emerald Group Publishing | 2000
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