FIELD: hypersonic aircraft.
SUBSTANCE: method for designing a hypersonic aircraft and a hypersonic aircraft designed using the method refer to means for designing structural elements of hypersonic aircraft (HAC), including unmanned aerial vehicles, using automated calculation of aerothermodynamic and thermal strength characteristics. The method for designing a hypersonic aircraft is carried out using a device for the design of hypersonic aircraft, consisting of an initialization unit, an external appearance research unit, a power plant research unit and a post-processing unit. The method for designing a hypersonic aircraft consists in creating a 3D model of the aircraft or power plant, creating a surface and volumetric mesh for the 3D model, conducting computational studies of the 3D model, visualizing a graphical representation of the results of the computational studies and generating a report on the computational studies performed.
EFFECT: method for designing a hypersonic aircraft and a hypersonic aircraft designed using the method make it possible to improve the aerodynamic quality.
1 cl, 2 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| METHOD FOR HYPERSONIC AIRCRAFT (HAC) MODEL ROLL ANGLE GENERATION OF A CONTROL SIGNAL FOR CONTROLLING THE AERODYNAMIC IDENTITY ACCORDING TO THE REYNOLDS NUMBERS OF THE FLIGHT TRAJECTORIES OF THE MODEL AND THE FULL-SCALE AIRCRAFT IN CONDUCTING ADVANCED FLIGHT TESTS OF AERODYNAMIC CHARACTERISTICS | 2017 |
|
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| AERODYNAMIC MODEL OF AIRCRAFT WITH INTEGRATED AIR BREATHING ENGINE | 2008 |
|
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| METHOD OF AIRCRAFT ENGINES CREATION | 2017 |
|
RU2726958C2 |
| METHOD OF DETERMINATION OF THE CONTROL SIGNAL ON THE CORNER OF THE ROLL MODEL OF THE HYPERPOWER VEHICLE EQUIPMENT (HVE) FOR MONITORING THE AERODYNAMIC IDENTITY ON THE REINOLDS NUMBER OF TRAJECTORIES OF THE FLIGHT OF THE MODEL AND THE NUCLEAR ARTICLE WHEN CONDUCTING ANTI-STATE AIRCRAFT RESEARCH | 2016 |
|
RU2615220C1 |
| SPECIALIZED SOFTWARE AND HARDWARE COMPLEX FOR COMPUTER-AIDED DESIGN OF RADAR STATIONS, COMPLEXES AND SYSTEMS, AS WELL AS THEIR COMPONENTS (SSHC) | 2021 |
|
RU2778139C1 |
| CYBER-PHYSICAL SYSTEM FOR RESEARCH OF FLIGHT CHARACTERISTICS OF AIRCRAFT | 2023 |
|
RU2804548C1 |
| FUSELAGE AIR BLEED FOR POWERING AIRCRAFT SYSTEMS | 2008 |
|
RU2361779C1 |
| METHODS OF DETERMINATION OF ATTACK ANGLES AND SLIDE AT FLIGHT TRIALS OF SUPERSONIC FLYING MACHINE | 2007 |
|
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| METHOD OF ESTIMATING THE EFFICIENCY OF INFORMATION MEANS OF ARMS WHEN DETECTING HCM AND A DEVICE WHICH IMPLEMENTS | 2019 |
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| TETHERED AIR HELICOPTER SIMULATOR | 2016 |
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