Results 121 to 130 of about 247 (153)

Improvement and verification of low-speed aerodynamic characteristics of a supersonic civil transport aircraft

Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, 2006
For supersonic civil transport aircraft, the low-speed aerodynamic characteristics form an important factor in its operational capabilities and in its economic viability. Low drag is a prerequisite to meet the present and future noise and emissions requirements.
exaly   +2 more sources

Sensitivity Analysis of Total Weight Parameters for Supersonic Civil Aircraft

Lecture Notes in Mechanical Engineering
Wei Wang, Yanxin Wei, Junfu Li, Yuting Tan, Yan Zhao, Junqiang Ai, Haochen Dong   +6 more
exaly   +2 more sources

Analysis of Flight Mechanics of a new Civil Supersonic Aircraft Conceptual Design [PDF]

The DLR-project STORMIE investigates novel concepts for supersonic passenger transport, with a particular focus on low boom characteristics. Three aircraft designs are being developed and analyzed for this purpose. This paper presents a flight mechanics analysis of one of these aircraft designs - a supersonic business jet - conducted during the early ...
Christmann, C., Sachs, F., Kirz, J.
openaire   +1 more source

Real-time obstacle detection system for high speed civil transport supersonic aircraft

Proceedings of the IEEE 2000 National Aerospace and Electronics Conference. NAECON 2000. Engineering Tomorrow (Cat. No.00CH37093), 2002
The High Speed Civil Transport (HSCT) supersonic commercial aircraft under development by National Aeronautics and Space Administration (NASA) and its partners is expected to include an eXternal Visibility System (XVS) to aid the pilot's limited view through their cockpit windows.
null Mau-Tsuen Yang, T. Gandhi, R. Kasturi, L. Coraor, O. Camps, J. McCandless   +5 more
openaire   +1 more source

Review of trajectory planning methods for civil supersonic aircraft

The Aeronautical Journal
Abstract Renewed interest in supersonic air travel has prompted researchers to reconsider the design and operation of supersonic transport aircraft. Previously, such aircraft were restricted to overwater routes due to the disturbances caused by their sonic booms.
M. Colling, P. Thomas, P. Sarhadi
openaire   +1 more source

Wind-Optimal Transatlantic Route Planning for Civil Supersonic Aircraft

Journal of Aircraft
Renewed interest in supersonic air travel has prompted researchers to consider where next-generation civil supersonic aircraft will operate. These aircraft are expected to fly lower and slower than Concorde, meaning that prevailing winds will have a greater impact on flight duration and fuel consumption. However, nonstandard atmospheric conditions have
Mike Colling, Peter R. Thomas, Pouria Sarhadi   +2 more
openaire   +1 more source

Optimal Fuel Consumption Trajectories of a Civil Supersonic Aircraft

Journal of Computer and Systems Sciences International, 2022
Kumakshev, S. A., Shmatkov, A. M.
openaire   +2 more sources

Turnable CO 2 laser measurements of composition and concentrations in multicomponent wake behind supersonic civil aircraft

SPIE Proceedings, 2005
The paper describes experimental and theoretical investigations on tunable CO2-laser-assisted measurements of the composition and concentrations in multicomponent wake behind supersonic civil aircraft. An experimental facility based on a tunable CO2 laser and multipass cell is presented and results of experiments on determination of substances typical ...
Sergey P. Ilyin, Anatoly A. Adamenkov, Evgeniy S. Asmolov, Yuri N. Bulkin, Boris A. Vyskubenko, Maxim Y. Deryugin, Yuriy V. Kolobyanin, Evgeniy A. Kudryashov, Dmitriy A. Rusyanov, Andrey V. Shustov   +9 more
openaire   +1 more source

SONIC BOOM CHARACTERISTICS UNDER STRONG ATMOSPHERIC TURBULENCE USING A SUPERSONIC CIVIL AIRCRAFT DEMONSTRATOR AS AN EXAMPLE

Акустический журнал / Acoustical Physics
Based on the wave equation exact within the framework of linear acoustics of moving media, a scalar equation on acoustic pressure in the atmospheric boundary layer is obtained. The main approximations for diffraction and turbulent pulsations transport effects are derived. Based on these, HOWARD and KZK-type models are developed. The two-dimentional KZK-
A. O. Korunov, S. Bakhne, L. A. Usov, A. I. Troshin, V. S. Gorbovskoy   +4 more
openaire   +2 more sources

Development of a quiet supersonic aircraft with technology applications to military and civil aircraft

40th AIAA Aerospace Sciences Meeting & Exhibit, 2002
S. Komadina, A. Drake, S. Bruner
openaire   +1 more source