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- W2089849168 abstract "The effect of descent rate (DR) on the approach aerodynamics of the F-15 S/MTD aircraft is investigated experimentally using a moving model in the NASA Langley Vortex Research Facility. A 0.083-scale low-speed rotary-balance model equipped with a thrust-reverser simulator and with grit strips to assure turbulent flow was tested in an approach configuration at forward speed 60 ft/sec, corresponding to DR = 4.19 ft/sec. The results are presented in extensive graphs and compared with wind-tunnel data on the same configuration at DR = 0. Significant differences are attributed to the DR in the present experiments and the presence of a ground boundary layer in the wind-tunnel tests. It is predicted that safe approaches could be made with the lower thrust reverser vectored up to 80 deg, or even 110 deg if the DR were not arrested near the ground." @default.
- W2089849168 created "2016-06-24" @default.
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- W2089849168 date "1989-08-14" @default.
- W2089849168 modified "2023-09-27" @default.
- W2089849168 title "A comparison of the ground effects measured with and without rate-of-descent modeling on the F-15 S/MTD configuration" @default.
- W2089849168 cites W1964807894 @default.
- W2089849168 doi "https://doi.org/10.2514/6.1989-3280" @default.
- W2089849168 hasPublicationYear "1989" @default.
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