Accession Number : AD0691915

Title :   AERODYNAMICS OF THE Mi-4 HELICOPTER

Corporate Author : AIR FORCE SYSTEMS COMMAND WRIGHT-PATTERSON AFB OH FOREIGN TECHNOLOGY DIVISION

Personal Author(s) : Yatsunovich, M S

PDF Url : AD0691915

Report Date : 13 Mar 1969

Pagination or Media Count : 371

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 :   *HELICOPTERS, AERODYNAMIC CHARACTERISTICS, FLIGHT, FLIGHT CONTROL SYSTEMS, HELICOPTER ROTORS, HOVERING, PERFORMANCE(ENGINEERING), USSR

Subject Categories : Aerodynamics
      Helicopters

Distribution Statement : APPROVED FOR PUBLIC RELEASE