FIELD: aircraft engineering.
SUBSTANCE: aerodynamic profile of the load-bearing element includes upper and lower contours formed by convex curves and their intersection points with given coordinates relative to the profile chord, and has a rounded leading edge.
EFFECT: improved aerodynamic characteristics of profiles for the end and middle sections of propeller blades, improved flight data of the aircraft in hovering and forward flight, an acceptable low level of variable and constant loads in the load-bearing system, and aeroelastic stability in a wide range of flight speeds are achieved.
4 cl, 6 dwg, 1 tbl
| Title | Year | Author | Number |
|---|---|---|---|
| AERODYNAMIC PROFILE OF AIRCRAFT LIFTING ELEMENT | 2023 |
|
RU2808865C1 |
| AERODYNAMIC PROFILE OF AIRCRAFT LIFTING ELEMENT | 2023 |
|
RU2808523C1 |
| AERODYNAMIC PROFILE OF BEARING SURFACE CROSS-SECTION (VERSIONS) | 2014 |
|
RU2559181C1 |
| AERODYNAMIC PROFILE OF THE AIRCRAFT CARRIER ELEMENT | 2020 |
|
RU2752502C1 |
| AERODYNAMIC PROFILE OF CROSS SECTION OF LIFTING SURFACE AREA | 2014 |
|
RU2558539C1 |
| AERODYNAMIC PROFILE OF CROSS SECTION OF LIFTING SURFACE AREA (VERSIONS) | 2014 |
|
RU2547475C1 |
| AERODYNAMIC PROFILE OF THE AIRCRAFT CARRIER | 2021 |
|
RU2762464C1 |
| AERODYNAMIC PROFILE OF THE LIFTING ELEMENT OF THE AIRCRAFT | 2021 |
|
RU2769545C1 |
| BLADE PROFILE FOR FLYING VEHICLE MAIN ROTOR AND MAIN ROTOR BLADE OF SUCH PROFILE | 1998 |
|
RU2191717C2 |
| PROPELLER BLADE | 1996 |
|
RU2123453C1 |
