FIELD: aeronautical engineering. SUBSTANCE: fairing is made in form of front-mounted bodies of revolution at exponent of generatrix ranging from 0.69 to 0.81 and distance between axes of symmetry equal to 0.75 to 1.0 of the body diameter. Plates may move longitudinally from top of each body and are cut at tops. EFFECT: reduction of total drag at preset elongation and frontal area. 2 cl, 4 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| 0 |
|
SU1782219A3 | |
| SUPERSONIC LOW-NOISE AIRCRAFT WITH TANDEM WINGS | 2015 |
|
RU2605585C1 |
| METHOD OF DESCENT IN ATMOSPHERE OF MEMBER SEPARATED FROM HYPERSONIC VEHICLE POSSESSING AERODYNAMIC EFFICIENCY AND DEVICE FOR ITS REALIZATION | 1995 |
|
RU2086903C1 |
| SUPERSONIC AIRCRAFT | 1995 |
|
RU2100253C1 |
| SUPERSONIC CONVERTIBLE AIRPLANE WITH X-SHAPED WING | 2016 |
|
RU2632782C1 |
| METHOD OF ACTING ON FLOW PASSING AROUND SYSTEM OF BODIES | 1993 |
|
RU2085444C1 |
| DOUBLE SUPERSONIC CONVERGENT AIR INTAKE (DSCAI) | 2018 |
|
RU2687437C1 |
| POLYWEDGE PIERCER | 1990 |
|
SU1826415A1 |
| SUPERSONIC CONVERTIBLE AIRCRAFT | 2015 |
|
RU2605587C1 |
| SUPERSONIC CONVERTIPLANE WITH X-SHAPED WING | 2015 |
|
RU2621762C1 |
