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Aircraft
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title: AIAA Journal of Aircraft
Tomographic Reconstruction of Hypersonic Aircraft Flowfields in Large-Scale Wind Tunnel Experiments
Three-dimensional flowfield features around a hypersonic aircraft model were reconstructed using a computed tomography background
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Magnetic-Control Variable Stiffness and Damping Tail Support for a Wind-Tunnel Aircraft Model
To suppress random vibration of aircraft models during wind tunnel tests, a novel magnetorheological elastomer (MRE)-based device with
...Assessing the Impact of Metrics on the Choice of Prognostic Methodologies
Flowfield Analysis of Vortex Interactions During Large Sharp-Edged Gusts
Computational Study on the Flow Structure of the Prandtl-D Flying Wing
Reliability of Hypersonic Airfoil with Freeplay and Stochasticity via Nonlinear Energy Sink
Application of Time-Variant Systems Theory to the Unsteady Aerodynamics of Rotary Wings
This work employs the principles of time-variant systems theory to investigate the unsteady aerodynamics of rotary-wing configurations
...Implementation and Linearization of a Coupled Panel and Vortex Particle Method in State-Space Form
This paper describes the implementation and linearization of a coupled panel and vortex particle method in a state-variable form. More
...Novel Skin-Reinforcement Design by Cross–Longitudinal Layout Inspired by Dragonfly Wing
The objective of this study is to develop a novel aircraft design approach using biomimetics as an alternative to traditional airframes
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The tonal and broadband noise of an ultrahigh-bypass-ratio fan stage, which has been developed at École Centrale de Lyon, is studied
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The prediction and control of thermoacoustic instability play a crucial role in combustion systems. This paper presents a novel
...Subregional Differentiated Safety Factors Design Based on Nonprobabilistic Structural Reliability
The structural safety factor is an essential parameter in aircraft design, representing the ratio of the design load to the operating
...On Improving the Noise Reduction Performance of Trailing Edge Serrations by Extension
Waverider Design Using Osculating Method
Because of the requirements of payload capability, flight range, and maneuverability, hypersonic aircraft demand high aerodynamic
...Neutral Buoyancy Testing of Low-Gravity Fluid Management
Validated Dynamic Stall Simulation of Pitching Low Reynolds Number Airfoils
Deep dynamic stall is one of several complex behaviors that result in extreme variation of the aerodynamic loads on small wind turbine
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Using nano-sized energetic materials as fuel additives to hydrocarbon gel fuel has gained in popularity due to the advantages of higher
...Experimental Study of Trailing-Edge Bluntness Noise Reduction by Porous Plates
The acoustic and aerodynamic fields of blunt porous plates are examined experimentally in an effort to mitigate trailing-edge bluntness
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