SIMULATION AND OPTIMIZATION OF ULTRALIGHT HELICOPTER AERODYNAMIC CHARACTERISTICS

The simulation and optimization of the ultralight helicopter aerodynamic characteristics at the design stages and phases which permit to determine optimal values of the engine power and speed are performed.

Saved in:
Bibliographic Details
Main Authors: Viktor P. Zharov, Sergey P. Lisin
Format: Article
Language:Russian
Published: Don State Technical University 2012-08-01
Series:Advanced Engineering Research
Subjects:
Online Access:https://www.vestnik-donstu.ru/jour/article/view/585
Tags: Add Tag
No Tags, Be the first to tag this record!