Articles tagged with Hypersonic Airplanes
NTU Singapore has unveiled its first locally designed and built full-sized eVTOL aircraft technology demonstrator, combining aerodynamic efficiency with hovering capability. The aircraft was developed over three years by researchers and engineers, powered by NTU-designed electric motors and featuring eight lift rotors.
Single-crystal HfB2 nanorods exhibit enhanced mechanical properties, with a 4.1% increase in hardness and 37.6% improvement in fracture toughness. The nanorods also demonstrate excellent ablation resistance, impeding oxygen atom penetration and reducing mass ablation rates.
A team of UVA engineering students is testing a novel, low-cost design for hypersonic research using a miniature spacecraft technology. If successful, the project could save millions of dollars per test flight and pave the way for future academic research in hypersonic flight.
Scientists at Duke University have engineered materials capable of producing tunable plasmonic properties while withstand extremely high temperatures. The new high-entropy carbides can achieve improved communications and thermal regulation in aerospace technologies, including satellites and hypersonic aircraft.
A new $1 million project at UCF aims to understand how raindrops interact with hypersonic shock waves. Researchers will use computer simulations and experiments to predict conditions for safe hypersonic travel. The knowledge gained could prevent damage and improve rocket launch accuracy.
Researchers at RMIT University developed highly versatile, cost-effective 3D printed catalysts that could tackle the challenge of overheating in hypersonic aircraft. The new catalysts show promise for fuelling the future of hypersonic flight by simultaneously cooling the system.
Researchers have developed a new family of aerodynamic configurations, called Hypersonic I-shaped Aerodynamic Configurations (HIAC), which aim to improve the efficiency and lift of hypersonic aircraft. The designs feature an extra wing that captures high-pressure airflow, resulting in a significant increase in lift coefficient and drag...
Researchers propose a new aerothermoelastic analysis method for hypersonic flight vehicles, combining two-way coupling and unified hypersonic lifting surface theory. The method considers thermal conduction and structural elastic deformation to improve analytical precision and calculate flutter speed.
Researchers present a body-wing-blending configuration with double flanking air inlets layout to achieve high lift-to-drag ratio and volumetric efficiency. A novel forebody design methodology using rotating and assembling two waverider-based surfaces is also introduced.