Methods for Estimating Drag Polars of Subsonic Airplanes PDF
89 Pages·1973·4.65 MB·English
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Description:
The purpose of this text is to present methods for computing drag polars of conventional airplanes at Mach numbers below 1.0. The word conventional is to be interpreted such that airplanes with highly swept, low aspect ratio wings (Л > 35°; A Categories: Technique\\Transportation: Aviation Year: 1
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