Wind-tunnel Investigation of the Low-speed Static and Rotary Stability Derivatives of a 0.13-scale Model of the Douglas D-558-II Airplane in the Landing Configuration
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An investigation was undertaken to determine the characteristics of several basic types of thrust-reverser. Models of three types, target, tailpipe cascade, and ring cascade, were tested with unheated air. The effects of design variables on reverse-thrust performance, reversed-flow boundaries, and thrust modulation characteristics were determined.
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