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. (Modified author abstract)


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    Title :

    Aircraft Antiskid Analysis Verification and Refinement


    Contributors:

    Publication date :

    1973


    Size :

    364 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




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