Results 71 to 80 of about 457,397 (165)
Aerodynamic optimization design of aircraft at maneuver points based on discrete adjoint equations
Modern supersonic aircraft with low aspect ratio must achieve favorable subsonic and supersonic cruise efficiency and high maneuverability. However, conventional aerodynamic optimization has primarily focused on cruise lift-to-drag characteristics, with ...
Qisheng Chen +5 more
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The noise of next-generation supersonic civil aircraft can become a significant nuisance for the population in the vicinity of airports. This study investigates the efficiency of the noise control approach for a notional supersonic civil aircraft at ...
Victor Kopiev +2 more
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Impact of Supersonic Aircraft on Upper Layers of (Atmosphere) Stratosphere
Recent scientific research have continued to assume thataircraft may contribute to the adverse chemical changes in theglobal atmosphere, especially regarding ozone (03) depletionas well as in possible changes in climate.Howeve1; there is substantial ...
Jasna Golubić +2 more
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Achieving global range in future subsonic and supersonic airplanes
No commercial airplane in service today is able to fly half great-circle distances over the globe and achieve the non-stop or the global range to any antipodal location on Earth.
Nihad E Daidzic
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The development of supersonic aircraft presents significant challenges in ensuring safety during early design stages, particularly for fuel tank systems exposed to extreme thermal and structural loads.
Ayush Kamboj, Yicheng Sun
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Do supersonic aircraft avoid contrails? [PDF]
The impact of a potential future fleet of supersonic aircraft on contrail coverage and contrail radiative forcing is investigated by means of simulations with the general circulation model ECHAM4.L39(DLR) including a contrail parameterization.
A. Stenke, V. Grewe, S. Pechtl
doaj
Modern problems of aircraft aerodynamics
The article represents the discussion of several separate directions of investigations, which are performed by TsAGI flight vehicles aerodynamics specialists at the time.
Sergey L. Chernyshev +2 more
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Installation Effects of Supersonic Inlets on Next-Generation SST Turbofan Engines
This study explores inlet-related installation effects on next-generation SST aircraft, focusing on supersonic business jets. Using a comprehensive framework with consistent thrust/drag bookkeeping and realistic modeling of inlet losses, including ...
Stylianos Adamidis +4 more
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Optimal design for low sonic boom based on CoKriging surrogate model
Accurately predicting and effectively reducing sonic boom levels is one of the key issues in the development of the new generation of green supersonic civil aircraft.
ZHANG Hanqi, XU Yue, ZHONG Min, LI Yan
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Nonlinear aerodynamics complexities of trending supersonic fighter aircraft entail formulation of a robust and reliable System Identification (Sys ID) technique that is capable of giving deep insight into its nonlinear characteristics and being self ...
Muhammad Fawad Mazhar +6 more
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