Results 11 to 20 of about 405 (198)

Implementation of Multidisciplinary and Multifidelity Uncertainty Quantification Methods for Sonic Boom Prediction

open access: yesJournal of Aircraft, 2023
To advance a supersonic aircraft design process, an uncertainty quantification study is conducted for sonic boom prediction while considering uncertainties associated with flight and atmospheric conditions. The uncertainty quantification process is implemented within a multidisciplinary analyses framework and assisted with a multifidelity surrogate ...
Huseyin Emre Tekaslan   +3 more
openaire   +3 more sources

Sonic Boom Focusing Prediction and Delta Wing Shape Optimization for Boom Mitigation Studies

open access: yes, 2007
Supersonic travel over land would be a reality if new aircraft are designed such that they produce quieter ground sonic booms, no louder than 0.3 psf according to the FAA requirement. An attempt is made to address the challenging goal of predicting the sonic boom focusing effects and mitigate the sonic boom ground over pressure for delta wing geometry.
Khasdeo, Nitin
openaire   +4 more sources

Sonic Boom Prediction Using Euler/Full Potential Methodology

open access: yes, 2005
Sonic Booms of two different bodies, a double cone configuration and a modified F-SE aircraft, are predicted using Euler solvers for the near field, and a Full Potential Propagation method for the far field. The problem is considered inviscid since viscous effects in high Reynolds number flows are negligible in Sonic Boom propagation.
Ozcer, Isik Ali
openaire   +4 more sources

Deep learning for inverse design of low-boom supersonic configurations

open access: yesAdvances in Aerodynamics, 2023
Mitigating the sonic boom to an acceptable stage is crucial for the next generation of supersonic transports. The primary way to suppress sonic booms is to develop a low sonic boom aerodynamic shape design.
Shusheng Chen   +4 more
doaj   +1 more source

Influence of Quiet Spike on Supersonic Transport for Low Boom Effect

open access: yesXibei Gongye Daxue Xuebao, 2019
One of the biggest technical challenges of supersonic flight is the mitigation of sonic boom. To deal with this problem, the Gulfstream Aerospace Corporation came up with the spike concept, and it showed to be efficient.

doaj   +1 more source

Optimal design for low sonic boom based on CoKriging surrogate model

open access: yesHangkong gongcheng jinzhan
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
doaj   +1 more source

Prediction of sonic boom overpressures near lateral cutoff [PDF]

open access: yesThe Journal of the Acoustical Society of America, 1992
Two methods of sonic boom predictions are used to compare predicted overpressures to measured sonic booms to quantify the effects of weather and flight variability on the lateral propagation of the booms. The sonic boom measurements were collected by the US Air Force at Edwards AFB, CA using a variety of supersonic aircraft.
J. Micah Downing, Robert A. Lee
openaire   +1 more source

Ground elevation effects on sonic boom reflection

open access: yes, 2020
International audienceSonic boom prediction is tackled within the EU projectRUMBLE. Its aim is to determine the acceptable level ofoverland sonic booms and the appropriate ways to complywith it [1].
Blanc-Benon, Philippe   +3 more
core   +1 more source

Sonic boom and drag evaluation of supersonic jet concepts [PDF]

open access: yes, 2018
This paper evaluates three different class supersonic airliners (Concorde, Cranfield E-5, and NASA QueSST X-plane) in a multidisciplinary design analysis optimization (MDAO) environment in terms of their sonic boom intensities and aerodynamic performance.
Howard Smith   +3 more
core   +1 more source

Multidisciplinary Design Optimization for the Conceptual Design of Supersonic Civil Aircraft Based on Full-Carpet Sonic Boom/Aerodynamic Characteristics Employing Differential Evolution

open access: yesAerospace
Reducing the sonic boom intensity and increasing the cruise lift-to-drag ratio are pivotal technologies for the successful development of supersonic civil aircraft.
Yuyu Duan   +3 more
doaj   +1 more source

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