Aircraft Antiskid Analysis Verification and Refinement

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.

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Document Details

Document Type
Technical Report
Publication Date
Sep 01, 1973
Accession Number
AD0770300

Entities

People

  • Byron H. Anderson

Organizations

  • General Dynamics

Tags

Communities of Interest

  • Air Platforms
  • Counter WMD
  • Sensors
  • Space

DTIC Thesaurus Topics

  • Aerodynamic Characteristics
  • Aircraft Equipment
  • Aircrafts
  • Brake Fluids
  • Computer Programs
  • Control Surfaces
  • Control Systems
  • Detectors
  • Elastic Properties
  • Fluid Flow
  • Landing Gear
  • Measurement
  • Nose Wheels
  • Steady State
  • Test And Evaluation
  • Three Dimensional
  • Two Dimensional

Readers

  • Aviation Science / Aeronautics.
  • Computational Modeling and Simulation
  • Logistics and Supply Chain Management.