1980•NASA STI Repository (National Aeronautics and Space Administration)Open access
High-speed T-38A landing gear extension loads
Andreas Schmitt
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Abstract
Testing of T-38A landing gear extension at high speed and high altitude is described. The mechanisms are shown together with peak hydraulic pressure data during landing gear deployment with active and inactive strut door flaps. Results of strain gage measurements of stress on various structural members are included.
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