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According to BRITISH EXPERIMENTAL TUEBOJET AIRCRAFT,Barry Jones, CROWOOD AVIATION SERIES, Page 198,


"A conical, fixed centre-body occupied the top portion of the intake, which had the first 15in(40cm) of its lip able to slide forward when the undercarriage was lowered, to allow for the engine's pressure recovery at landing speed, and sliding back to the in-flight position once the wheels had been retracted. "


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