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
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
...On Improving the Noise Reduction Performance of Trailing Edge Serrations by Extension
Neutral Buoyancy Testing of Low-Gravity Fluid Management
Waverider Design Using Osculating Method
Because of the requirements of payload capability, flight range, and maneuverability, hypersonic aircraft demand high aerodynamic
...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
...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
...Data Fusion of Wing Pressure Distributions Using Scalable Gaussian Processes
Aircraft design requires a large volume of aerodynamic data to characterize various flight conditions throughout the aircraft’s flight
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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
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Ceramic matrix composites (CMCs) are the core strategic materials for the thermal structure of new-generation hypersonic aircraft. The
...On the Use of Lifting Line Approaches for Propellers with Large Chord Variations