1. Concept", AIAA98-3256.
2. "Aircraft Thrust Reverser Cascade Configuration
3. Symposium, 239c, Montreal,Canada, 2003. Fig. 1 SchematicDiagramof ThrustReverser (a) Earlyseparation fromdiverter fairing atlowpressureintranscowlcavity (b) Later separationfromdiverter fairing athighpressureintranscowlcavity