FIELD: wings and lifting surfaces of wing-in-ground-effect machines. SUBSTANCE: range of lift coefficients Cst is extended; inherent stability of wing profile of wing-in-ground-effect machine is ensured at altitudes both at heavy ((H<0,4BA)) and weak ((H>0,4BA)) screen effect. Aerodynamic profile has nose 4, trailing-edge piece 5 connected by means of upper contour 1 and lower contour 3 forming S-shaped center line 3. Maximum thickness CHmax of lower contour 2 is located at distance lesser than 0.7 of chord BA from nose 4 of profile and lower contour 2 of trailing-edge piece 5 is convex at distance of (0,1...0,3)BA from trailing-edge piece 5 at curvature radius of Rh.ed.low = (0,5...4,5)BA.. Lower contour 2 of profile may have at least one rectilinear section; curvature radius Rh.ed.low of lower contour may be constant and varying (reducing towards trailing-edge piece 5). EFFECT: extended range of lift coefficients. 5 cl, 4 dwg
Title | Year | Author | Number |
---|---|---|---|
METHOD FOR STABILISATION OF FLIGHT OF RAM WING SURFACE EFFECT VEHICLE AND RAM WING SURFACE EFFECT VEHICLE IMPLEMENTING THIS METHOD | 2013 |
|
RU2546048C1 |
GROUND-EFFECT VEHICLE | 2019 |
|
RU2716303C1 |
TRANSPORT SYSTEM (VERSIONS), AIRFOIL TRAIN AND GUIDING RAIL FOR IT | 2010 |
|
RU2463182C2 |
EKRANOPLAN OF INTEGRATED AEROGYDRODYNAMIC COMPOUND | 2016 |
|
RU2629463C1 |
AIR-CUSHION VEHICLE - THE VEHICLES CARRIER | 2017 |
|
RU2658545C1 |
WING-IN-GROUND-EFFECT CRAFT | 2003 |
|
RU2286268C2 |
METHOD OF STABILIZATION OF WING-IN-GROUND EFFECT CRAFT AND WING-IN-GROUND EFFECT CRAFT FOR REALIZATION OF THIS METHOD | 1995 |
|
RU2097269C1 |
HOVERCRAFT | 2011 |
|
RU2466888C1 |
MECHANIZATION OF LIFTING SURFACE OF DYNAMIC AIR CUSHION VEHICLE | 1997 |
|
RU2127203C1 |
ELECTRIC AMPHIBIAN AIRFOIL BOAT | 2019 |
|
RU2737406C1 |
Authors
Dates
1998-08-27—Published
1997-07-02—Filed