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):

• Yatsunovich, M. 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:

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

Subject Categories:

• Aerodynamics
• Helicopters

Distribution Statement:

APPROVED FOR PUBLIC RELEASE