Title:
超音速自然層流翼
Document Type and Number:
Japanese Patent JP3668493
Kind Code:
B2
Abstract:
A reverse delta aerodynamic wing has a basic reverse delta wing portion bounded by a leading edge and by a pair of trailing edges extending from respective ends of said leading edge toward a trailing apex point and respective span-wise wing extensions in a natural laminar boundary layer wing region extending chordwise from said leading edge by a fraction of the chordlength of said wing and extending span-wise from opposing sides of said wing. Laminar flow control in other regions of the wing employs fuel stored in the wing as a coolant.
Inventors:
Gear Heart, Heinz A
Application Number:
JP51701395A
Publication Date:
July 06, 2005
Filing Date:
December 14, 1994
Export Citation:
Assignee:
NORTHROP GRUMMAN CORPORATION
International Classes:
B64C3/10; B64C3/36; B64C9/14; B64C21/00; B64C30/00; (IPC1-7): B64C3/10; B64C30/00
Foreign References:
| US1843678 |
Attorney, Agent or Firm:
Kazuo Moriya