FIELD: transport.
SUBSTANCE: group of inventions relates to application of airfoils. Proposed method comprises forming of confuser on the wing leading edge by extra airfoil to be arranged under wing nose part. Note here that updated aircraft wing of known design is used. Extra airfoil is selected from the list including: fixed profile, all-moving profile, rotary profile with different pivot pins, split profile and all-extending profile. Wing is updated in compliance with proposed method.
EFFECT: increased lift.
4 cl, 8 dwg
| Title |
Year |
Author |
Number |
| METHOD FOR CREATION OF ADDITIONAL REACTIVE JET AND LOWERING WAVE IMPEDANCE FOR MOVABLE, FOR INSTANCE LAUNCHED, BODY IN FORM OF MISSILE WITH PREDOMINANTLY OGIVAL OR SHARP-POINTED NOSE AND MISSILE-SHAPED BODY WITH PREDOMINANTLY OGIVAL OR SHARP-POINTED NOSE |
2012 |
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|
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|
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2012 |
- Il'In Aleksej Valentinovich
|
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|
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|
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2003 |
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|
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2013 |
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|
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|
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