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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
Computational Study on the Flow Structure of the Prandtl-D Flying Wing
Flowfield Analysis of Vortex Interactions During Large Sharp-Edged Gusts
Reliability of Hypersonic Airfoil with Freeplay and Stochasticity via Nonlinear Energy Sink
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
...Waverider Design Using Osculating Method
Because of the requirements of payload capability, flight range, and maneuverability, hypersonic aircraft demand high aerodynamic
...On Improving the Noise Reduction Performance of Trailing Edge Serrations by Extension
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
...Neutral Buoyancy Testing of Low-Gravity Fluid Management
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
...Mitigation of Roughness-Induced Boundary-Layer Transition on Airfoils Using Shielding Strips
Boundary-layer transition in the wake of a discrete roughness element results in a turbulent wedge that can adversely affect aerodynamic
...Transonic Flutter of Skin Panels Pinned at the Center
This work is a numerical and experimental study of transonic panel flutter. Two configurations were explored: clean and pinned geometry
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