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- W165114966 abstract "An investigation has been conducted in the Langley 16-Foot Transonic Tunnel to determine the effects on empennage arrangement on single-engine nozzle/afterbody static pressures. Tests were done at Mach numbers from 0.60 to 1.20, nozzle pressure ratios from 1.0 (jet off) to 8.0. and angles of attack from -3 to 9 deg (at jet off conditions), depending on Mach number. Three empennage arrangements (aft, staggered, and forward) were investigated. Extensive measurements were made of static pressure on the nozzle/afterbody in the vicinity of the tail surfaces." @default.
- W165114966 created "2016-06-24" @default.
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- W165114966 date "1987-11-01" @default.
- W165114966 modified "2023-09-24" @default.
- W165114966 title "Effect of empennage arrangement on single-engine nozzle/afterbody static pressures at transonic speeds" @default.
- W165114966 hasPublicationYear "1987" @default.
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