Canard position and dihedral for boom reduction and...

Details Canard position and dihedral for boom reduction and... Canard position and dihedral for boom reduction and...

2005-06-07

2008-08-26

Collins, Timothy D (Department: 3643)

Aeronautics and astronautics

Aircraft sustentation

Sustaining airfoils

C244S00100R

Reexamination Certificate

active

07416155

ABSTRACT:
A supersonic aircraft comprises a fuselage extending forward and aft, wings coupled to lateral sides of the fuselage, and canards coupled to lateral sides of the fuselage forward of the wings. The individual canards are configured to generate shocks that wrap around the fuselage and intersect with wing leading edges on opposing sides of the fuselage.

REFERENCES:
patent: 6729577 (2004-05-01), Morgenstern
http://www.faqs.org/docs/air/avgrpn.html, the gripen aircraft.

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