Calculations of responses to continuous turbulence of B-47A airplane were compared with flight test results; calculations, based on 5° of freedom, lifting-surface aerodynamics for non-steady subsonic flow, and one-dimensional turbulence agree favorably with flight test results; method of calculation should give results of corresponding accuracy when applied to similar configurations.
Calculated responses of large sweptwing airplane to continuous turbulence with flight-test comparisons
NASA -- Tech Report
1960
14 pages
Report
English
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