Browse TRAIL Inventories

Effect of elevator-profile modifications and trailing-edge strips on elevator hinge-moment and other aerodynamic characteristics of a full-scale horizontal tail surface

Tests of a full-scale horizontal tail surface in the Langley 16-foot high-speed tunnel

Pressure-distribution measurements on a full-scale horizontal tail surface for a Mach number range of 0.20 to 0.70

Analytical and experimental investigation of inlet-engine matching for turbojet-powered aircraft at Mach numbers up to 2.0

An inlet design concept to reduce flow distortion at angle of attack


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