Accession Number:
AD0691915
Title:
AERODYNAMICS OF THE Mi-4 HELICOPTER
Descriptive Note:
Corporate Author:
AIR FORCE SYSTEMS COMMAND WRIGHT-PATTERSON AFB OH FOREIGN TECHNOLOGY DIVISION
Personal Author(s):
Report Date:
1969-03-13
Pagination or Media Count:
371.0
Abstract:
The report describes the aerodynamics of single-rotor helicopters. The practical aerodynamics of the Mi-4 helicopter are analyzed. The rotor is analyzed in detail as well as flight conditions and other aerodynamic characteristics.
Descriptors:
Subject Categories:
- Aerodynamics
- Helicopters