Tests were conducted on a full scale Sikorsky CH-34 rotor blade system, instrumented to measure chordwise pressure distributions. The basic pressure measurements are presented in tabular form to make the detailed data available for possible analysis. (Author)
Tabulated Sikorsky CH-34 Blade Surface Pressures Measured at the NASA/Ames Full Scale Wind Tunnel
1966
2 pages
Report
Keine Angabe
Englisch
FULL-SCALE 1903 WRIGHT FLYER WIND TUNNEL TEST RESULTS FROM THE NASA AMES RESEARCH CENTER
British Library Conference Proceedings | 2000
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