The Effects Of Compressibility On The Upwash At The Propeller Planes Of A Four Engine Tractor Airplane Configuration Having A Wing With 40 Degrees Of Sweepback And An Aspect Ratio Of 10
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The Effects of Compressibility on the Upwash at the Propeller Planes of a Four-engine Tractor Airplane Configuration Having a Wing with 40 Degrees of Sweepback and an Aspect Ratio of 10
The results indicate that for Mach numbers up to 0.60 the upwash angles can be predicted accurately by the available theoretical methods. At Mach numbers above 0.60 the experimental values were less than those predicted by theory and this difference increased with increasing Mach number.