Abstract A technique is proposed of calculating the characteristic flight velocities for an airplane with taking into account the nominal performance of a piston engine. We consider an algorithm of design calculation for the airscrew blade geometry (twist angle, chord and optimal angle of attack along blade). Feasible rational versions of design parameters are discussed.
Algorithm of calculating the light airplane flight performance and rational design airscrew parameters at the preliminary design stage
Russian Aeronautics (Iz VUZ) ; 59 , 3 ; 364-370
2016-07-01
7 pages
Article (Journal)
Electronic Resource
English
AIAA | 2016
|Engineering Index Backfile | 1933
|Engineering Index Backfile | 1949
|Engineering Index Backfile | 1949
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