Accession Number:

AD0627133

Title:

PRELIMINARY FLIGHT TEST DATA UH-1B HIGH PERFORMANCE HELICOPTER

Descriptive Note:

Technical Report

Corporate Author:

ARMY TRANSPORTATION RESEARCH COMMAND FORT EUSTIS VA FORT EUSTIS United States

Personal Author(s):

Report Date:

1964-11-01

Pagination or Media Count:

32.0

Abstract:

This report presents the results of flight investigations conducted in association with the primary flight test investigation of the high performance UH-1 helicopter. Results reported include main rotor blades with inboard trailing edge flaps, a two-bladed flex beam rotor, and tapered tip main rotor blades.

Subject Categories:

  • Attack and Fighter Aircraft

Distribution Statement:

APPROVED FOR PUBLIC RELEASE