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Simulated Landing Approaches of an Unaugmented C-5A Configuration

Report Number: AFFDL TR 65-210
Author(s): F. D. Newell; M. L. E. Parrag; G. Bull
Corporate Author: Cornell Aeronautical Laboratories
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1966-03
Pages: 82
Contract: AF 33(615)-2411
Project: 8219
Task: 821905
AD Number: AD0482810

Expected ranges of unaugmented longitudinal and lateral-directional handling qualities of the C-5A class airplane were simulated and evaluated in a variable-stability B-26 for the instrument-landing.

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