Accession Number:

AD0770300

Title:

Aircraft Antiskid Analysis Verification and Refinement

Descriptive Note:

Final rept. Dec 1970-Arp 1973

Corporate Author:

GENERAL DYNAMICS FORT WORTH TX CONVAIR AEROSPACE DIV

Personal Author(s):

Report Date:

1973-09-01

Pagination or Media Count:

364.0

Abstract:

A program for verifying and refining a previously developed aircraft antiskid performance and system compatibility analysis procedure is described. Analysis verification was performed by comparing antiskid system operation as predicted by the analytical procedures with that recorded during laboratory testing. The laboratory tests were conducted at the Air Force Flight Dynamics Laboratory Landing Gear Test Facility at Wright-Patterson Air Force Base, Ohio using a set-up consisting of F-111 aircraft main landing gear, tire, wheel, brake, hydraulic brake actuation system and several antiskid control circuit variations.

Subject Categories:

  • Attack and Fighter Aircraft

Distribution Statement:

APPROVED FOR PUBLIC RELEASE