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- W2065929059 abstract "This paper summarizes the results of a force, moment, and pressure experiment involving six thick, cambered and twisted, delta wings with 58 deg leading-edge sweep. The goal of this study was to determine a configuration that was self-trimming at a design lift coefficient of 0.25 and Mach number of 0.80. Analysis of the forces and moments data did not indicate a configuration that satisfied the design constraints; however, the configuration that came closest and had the best overall performance was selected for detailed pressure study. Wing pressure data and limited surface oil-flow photographs for this configuration showed attached flow at the design point. The associated inviscid forces and moments solutions from the Vortex Lattice Method-Suction Analogy, PAN AIR, FLO-28, and FLO-57 were compared with experimental data and showed varying levels of success. The computed pressures obtained from the PAN AIR, FLO-28, and FLO-57 for an angle of attack of 6.08 deg underpredicted the measured upper-surface pressure peak. At higher angles of attack, the lower-surface theoretical and measured pressure data compared well, whereas the upper-surface pressure predictions only approximated the trends but not the pressure level. Of the three codes, the PAN AIR is shown to be the best overall predictor." @default.
- W2065929059 created "2016-06-24" @default.
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- W2065929059 date "1988-01-01" @default.
- W2065929059 modified "2023-09-26" @default.
- W2065929059 title "Force and pressure study of thick cambered/twisted 58 deg delta wings" @default.
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- W2065929059 doi "https://doi.org/10.2514/3.45543" @default.
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