Accession Number:

AD0477909

Title:

PRELIMINARY FLIGHT TEST DATA. XH-51A RIGID ROTOR HIGH SPEED FLIGHT PROGRAM

Descriptive Note:

Interim report no. 4

Corporate Author:

ARMY TRANSPORTATION RESEARCH COMMAND FORT EUSTIS VA

Personal Author(s):

Report Date:

1964-10-01

Pagination or Media Count:

30.0

Abstract:

This report summarizes the flight test results of the three-bladed rotor testing on the XH-51A rigid rotor helicopter. The object of this testing was to obtain data on maneuver limits and center-of-gravity offsets needed to proceed with the high speed flight testing of the XH-51A with wing and jet pod installed. A total of 39 flights were made with 11.6 hours of flight time during this testing.

Subject Categories:

  • Aerodynamics
  • Helicopters

Distribution Statement:

APPROVED FOR PUBLIC RELEASE