Flutter prediction, suppression and control in aircraft composite wings as a design prerequisite: a survey [PDF]
, 2007 Emergence of flutter compromises not only the long-term durability of the wing structure, but also the operational safety, flight performance and energy efficiency of the aircraft. Effectual means of flutter prevention are, therefore, mandatory in the
Njuguna, James A. K.
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Aerodynamics of variable geometry wing/body combinations [PDF]
A description of the experimental investigation of the aerodynamic characteristics of variable geometry of an aircraft model is presented. Aerodynamically, the model is tested-for a sweep range of 0°,12.5° 32.5°, and 52.5° and incidence range of 0° to ...
Ostadsaffari, A
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Identification and attenuation of slat noise [PDF]
, 2012 In the case of civil transport aircraft, engines were the dominant noise source until the advent of the high-bypass ratio engines in the early 1970s. Since then, airframe noise has become more important, particularly during the approach-to-landing stage ...
Chen, Peng
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Application of panel methods for subsonic aerodynamics
, 1985 Several panel methods are developed to model subsonic aerodynamics. The vorticity panel method for two-dimensional problems is capable of handling general unsteady, potential, lifting flows.
Kim, Meung Jung
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A Novel Airframe Design Methodology For Silent Aircraft [PDF]
, 2008 The impact of noise on civil aviation is not just a localised airport problem, but a global concern, due to the ever-increasing demands for passenger travel.
Mistry, Sunil
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Dimensionless Groups by Entropic Similarity: II-Wave Phenomena and Information-Theoretic Flow Regimes. [PDF]
Entropy (Basel), 2023 Niven RK.
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, 1998 Recent developments on a general boundary integral formulation for the aerodynamic and aeroacoustic analyses of lifting bodies (e.g., wings and rotors) are reviewed.
Gennaretti M +3 more
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Modelling & integration of advanced propulsion systems [PDF]
, 2008 This research study focuses on the design of advanced propulsion cycles, having as primary design goal the improvement on noise emissions and fuel consumption.
Doulgeris, Georgios C.
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Dataset of numerical simulations for aeroelastic control of an aero engine compressor cascade using plasma actuators. [PDF]
Data Brief, 2021 De Giorgi MG +3 more
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Numerical study on the influence of wall temperature gradient on aerodynamic characteristics of low aspect ratio flying wing configuration. [PDF]
Sci Rep, 2021 Lin P +6 more
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