Mechanical Behavior of Bistable Bump Surface for Morphing Inlet

There exists inlet-engine match conflict between high and low speeds for a non adjustable bump inlet. A scheme of using a bistable bump surface at the throat region of the inlet is proposed to adjust the throat area. The FEM model of the bistable surface is established with hinged constraint, and th...

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Veröffentlicht in:	Transactions of Nanjing University of Aeronautics & Astronautics 2015-12, Vol.32 (6), p.610-622
1. Verfasser:	张平 周丽 程文杰
Format:	Artikel
Sprache:	eng
Schlagworte:	Adjustment Bistability Energy use Inlets Mathematical models Parameters Structural strain Throats
Online-Zugang:	Volltext
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