Accession Number:

AD0781477

Title:

Pretest Information for the Directionally-Controlled Antitank Ring Wing Gyro Canard in the 16T of AEDC.

Descriptive Note:

Technical rept.,

Corporate Author:

ARMY MISSILE COMMAND REDSTONE ARSENAL ALA AEROBALLISTICS DIRECTORATE

Personal Author(s):

Report Date:

1974-04-24

Pagination or Media Count:

17.0

Abstract:

A test program is presented for the directionally-controlled antitank ring wing gyro canard mechanism. The purpose of the Arnold Engineering Development Center 16T wind tunnel test is to obtain photographic precessional data on the ring wing gyro mechanism over the angle of attack range -3 deg or alpha or 5 deg and Mach number range 0.3 or Mach number or 0.9 for Reynolds number 2,000,000. Author

Subject Categories:

  • Ammunition and Explosives
  • Fluid Mechanics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE