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- W2019988206 abstract "Aerodynamic characteristics obtained in a rotational flow environment, utilizing a rotary balance are presented in plotted form for a 1/12 scale F-15 airplane model. The configurations tested included the buildup of airplane components and the basic airplane with various control deflections. Data are presented for all configurations without analysis for an angle of attack range of 8 to 90 deg, and clockwise and counterclockwise rotations covering an omega b/2V range from 0 to 0.4. Selected configurations are presented over an extended omega b/2V range from 0 to 0.9." @default.
- W2019988206 created "2016-06-24" @default.
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- W2019988206 date "1982-05-01" @default.
- W2019988206 modified "2023-09-27" @default.
- W2019988206 title "F-15 rotary balance data for an angle-of-attack range of 8 deg to 90 deg" @default.
- W2019988206 hasPublicationYear "1982" @default.
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