EASY-ACLS Dynamic Analysis Volume I - Component Mathematical Methods

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Report Number: AFFDL TR 79-3105 Volume I
Author(s): Wahi, M. K., Kilner, J. R., Perkins, P. R., Duleba, G. S.
Corporate Author(s): Boeing Aerospace Company
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1979-09
Pages: 248
Contract: F33615-77-C-3054
DoD Task:
Identifier: ADA080634

Mathematical models were developed for a variety of Air Cushion Landing System components which include aircraft flight model components, wind, engine and air flow components, inelastic-elastic-trunk and cushion, air bag skid and arresting gear model components etc. The models were developed for utilization in the EASY-ACLS dynamic analysis computer program simulation.

Provenance: Bombardier/Aero

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