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Pusher configuration
A Numerical Approach for Implementing Air Intakes in a Canard Type Aircraft for Engine Cooling Purposes
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Wind-Tunnel Investigation of the Flight Chasacteristics of a Canard
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Wind-Tunnel Investigation of the Flight Chasacteristics of a Canard Genera1:Aviation Airplane Coniiguration
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Numerical Analysis of the Effect of Fuselage of Fan-In-Body Aircraft on the Pusher Propeller
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Conceptual Design of UAV at Low Reynolds Number and High Payload Lifting Canard Configuration
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Configuration Redesign and Prototype Flight Testing of an Unmanned Fixed- Wing Evtol Aircraft with Under-Fuselage Hover Lift and Pusher Wingtip Propulsion System
Propeller Installation Effects on Turboprop Acoustics
Changes in Propeller Performance Due to Ground and Partial
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Cranfield University Pablo Bellocq Multi-Disciplinary Preliminary Design Assessments of Pusher Counter-Rotating Open Rotors