Analysis of Flight-Determined and Predicted Effects of Flexibility on the Steady-State Wing Loads of the B-52 Airplane
1958
62 pages
Report
No indication
English
Aircraft , B- 52 aircraft , Flexibility , Wing loading , Aeroelasticity , Determination , Effect , Flight , Lift , Loading , Mach number , Prediction , Pressure , Steady state , Structure , Velocity , Wing
Engineering Index Backfile | 1957
|Engineering Index Backfile | 1958
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