Synonyme wurden verwendet für:
Aircraft
Suche ohne Synonyme:
title: AIAA Journal of Aircraft
Inverse Design Method for Low-Boom Supersonic Transport with Lift Constraint
The low-boom inverse design method is of great interest for the preliminary design of supersonic transport (SST), owing to its good
...Simulating Airplane Aerodynamics with Body Forces: Actuator Line Method for Nonplanar Wings
Two configurations typical of fixed-wing aircraft are simulated with the actuator line method (ALM): a wing with winglets, and a T tail
...Numerical Study on Wind-Driven Thin Water Film Runback on an Airfoil
Fluidic-Oscillator-Based Pulsed Jet Actuation on a Vertical Tail
This paper investigates the performance, aerodynamics, and aeroacoustics of NASA’s side-by-side urban air mobility (UAM) aircraft in
...Novel High-Precision and Efficient Momentum Source Method
Improved Dynamic Geometry Control Algorithms for Efficient Aerodynamic Shape Optimization
Pulsed Velocity Created by a Plasma Actuator in the Vicinity of the Wall
Force/Moment-Conserving Pressure Mapping Scheme for Fluid/Structure Interaction Analysis
Flow Topology of a Slanted Cylinder with Rounded-Edges Under Compressible Conditions
In this study, the slanted afterbody was modified to more closely represent cargo aircraft afterbodies through the addition of a basal
...Deep-Learning Strategy Based on Convolutional Neural Network for Wall Heat Flux Prediction
Aerodynamic thermal prediction plays an important role in the design of hypersonic aircraft, especially in the design of the aircraft’s
...Duct Effects on Acoustic Source Radiation
This paper presents a detailed numerical investigation of the effects of a semi-infinite hard-walled duct on the radiation due to point
...Vortex Identification and Quantification on Blunt Trailing-Edge Rotor Blades in Reverse Flow
An inherent aerodynamic limitation of high-advance-ratio high-speed helicopters is reverse flow on the retreating blades, which can be a
...Spatial Transformations for Reacting Gas Shock Tube Experiments
FFVHC-ACE: Fully Automated Cartesian-Grid-Based Solver for Compressible Large-Eddy Simulation
Equivalent Area Targets for Inverse Design Optimization With Changing Low-Boom Cruise Conditions
Three-Dimensional Quantitative Flow Visualization Around a Thrust Reverser