Simulated Landing Approaches of an Unaugmented C-5A Configuration
Report Number: AFFDL TR 65-210
Author(s): Newell, F. D., Parrag, M. L. E., Bull, G.
Corporate Author(s): Cornell Aeronautical Laboratories
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1966-03
Pages: 82
Contract: AF 33(615)-2411
DoD Project: 8219
DoD Task: 821905
Identifier: AD0482810
Abstract:
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.
Provenance: Lockheed Martin Missiles & Fire Control
Author(s): Newell, F. D., Parrag, M. L. E., Bull, G.
Corporate Author(s): Cornell Aeronautical Laboratories
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1966-03
Pages: 82
Contract: AF 33(615)-2411
DoD Project: 8219
DoD Task: 821905
Identifier: AD0482810
Abstract:
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.
Provenance: Lockheed Martin Missiles & Fire Control