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- W2750672610 abstract "Technique for relating transient tolerances in inlet throat Mach number and shock position to supersonic unstart frequency due to atmospheric turbulence for supersonic inlet design" @default.
- W2750672610 created "2017-09-15" @default.
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- W2750672610 date "1968-12-01" @default.
- W2750672610 modified "2023-09-25" @default.
- W2750672610 title "Development of atmospheric gust criteria for supersonic inlet design" @default.
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