FIELD: transportation.
SUBSTANCE: aerodynamic model comprises detachable head, stern and intermediate modules. Contours of modules imitate contours of aircraft body sections on a reduced scale, which are defined by conventional division of the latter in parts limited by shape and location of its lower or upper surfaces of the same type. At the same time external contours of modules are shaped by combination of surfaces of simple geometric figures.
EFFECT: suitability for tests on existing test bench equipment, low manufacturing cost, provision of tested models appearance versions expansion, high manufacturability.
25 cl, 2 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| LIQUIDISING PLANT FOR AIRCRAFT | 2012 |
|
RU2521124C1 |
| METHOD FOR RESEARCHING AND OPTIMISING CONFIGURATION OF AERIAL VEHICLE AND MODEL FOR IMPLEMENTATION THEREOF | 2020 |
|
RU2761543C1 |
| AERODYNAMIC MODEL OF AIRCRAFT WITH AIR-JET ENGINE | 2019 |
|
RU2726564C1 |
| COMBINED DYNAMICALLY SCALED AERODYNAMIC MODEL FOR DIFFERENT TYPES OF AERODYNAMIC TESTS | 2023 |
|
RU2808290C1 |
| FLYING VEHICLE WITH MIXED POWER PLANT | 1998 |
|
RU2130407C1 |
| LARGE-SIZED AERODYNAMIC MODEL | 2015 |
|
RU2607675C1 |
| RETURN MULTIMODE PILOTLESS AIRCRAFT WITH CHANGEABLE STATISTIC MARGIN | 2008 |
|
RU2384470C1 |
| AIRCRAFT AUXILIARY POWER UNIT AIR INTAKE MODEL FOR WIND TUNNEL TESTING | 2022 |
|
RU2793637C1 |
| METHOD OF CONDUCTING AERODYNAMIC TESTS ON MODEL AIRCRAFT AND STAND FOR REALISING SAID METHOD | 2009 |
|
RU2421701C1 |
| AEROSPACE CRAFT WITH NUCLEAR PROPULSOR AND AEROSPACE FLIGHTS PERFORMED THEREBY | 2013 |
|
RU2574295C2 |
