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JPS5493600A |
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JPS5477999A |
The present aircraft steering method makes use of additional lift gained by controlling the separating of vortical flows from the leading edges of the wings for the purpose of controlling the aircraft about its pitch axis, its roll axis,...
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JPS5433498A |
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JPS53109398A |
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JPS5334299A |
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JPS536436B1 |
1,079,296. V/STOL aircraft. DEHAVILLAND AIRCRAFT OF CANADA Ltd. Aug. 4, 1964 [Aug. 29, 1963], No. 31261/64. Heading B7G. [Also in Division F2] A vertical or short take-off and landing aircraft has wings provided with trailing edge flaps ...
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JPS5244120B2 |
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JPS52121297A |
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JPS51135100A |
A strake, or strakes, or faired simulation of same, mounted on a typical engine nacelle or similar wing mounted body to reduce or prevent the formation of vortices usually occurring with nacelle-wing combinations to improve the lift and ...
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JPS50156200A |
A means for attenuating the vortex created at aircraft wingtips which consists of a retractable planar surface transverse to the airstream and attached downstream of the wingtip which creates a positive pressure gradient just downstream ...
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JPS5019000B1 |
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JPS5055014A |
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JPS5047399A |
1441646 Aircraft S C RETHORST 27 Sept 1973 [16 March 1973] 45398/73 Heading B7W An aircraft has a wing 42 and a nozzle 52 having an outlet which is transversely elongate relative to the aircraft and through which in operation a supersoni...
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JPS49102100A |
A lift cell comprising an airfoil section or sections containing a plurality of airfoils enclosed within an enclosure and a device for forcibly moving air through the airfoil section or sections. The airfoils are shaped and arranged so t...
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JPS4914598B1 |
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JPS4914599B1 |
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JPS492760B1 |
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JPS4840238B1 |
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JPS4873998A |
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JPS4867999A |
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JPS4858599A |
An airfoil having an upper surface shaped to control flow accelerations and pressure distribution over the upper surface and to prevent separation of the boundary layer due to shock wave formulation at high subsonic speeds well above the...
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