Synonyme wurden verwendet für:
Waves
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keywords:(Mach Waves)
Shock train behavior affected by continuous Mach number variation of incoming flow
A method for predicting Mach stem height in steady flows
Nonlinear ion-acoustic waves at Venus ionosphere
Obliquely propagating ion-acoustic solitons and supersolitons in four-component auroral plasmas
Aerodynamic Phenomena in Supersonic Flow
Reduced-Order Comparison of Simulated and Measured Coalescing Mach Waves near Supersonic Jets
Numerical Algorithm for Computing Acoustic and Vortical Spatial Instability Waves
Temperature Effects on Convection Speed and Steepened Waves of Temporally Developing Supersonic Jets
Shock-Wave/Boundary-Layer Interaction Control Using Three-Dimensional Bumps for Transonic Wings
Planar Shock-Wave Diffraction into a Square Cavity Filled with Different Gases
Source Localization of Crackle-Related Events in Military Aircraft Jet Noise
Experimental Characterization of Supersonic Flow over a Wall-Mounted Hemisphere
Detonation Simulations in Supersonic Combustible Mixtures with Nonuniform Species
Antisymmetric Oscillation Modes in Rectangular Screeching Jets
Coherence Analysis of the Noise from a Simulated Highly Heated Laboratory-Scale Jet
Optical Measurements of Transitional Events in a Mach-6 Boundary Layer
Spatiotemporal-Correlation Analysis of Jet Noise from a High-Performance Military Aircraft
Overexpansion Effects on Characteristics of Mach Waves from a Supersonic Cold Jet
Excitation of Free Shear-Layer Instabilities for High-Speed Flow Control
Three-Way Spectral Decompositions of High-Performance Military Aircraft Noise
Studies on the Influence of Steady Microactuators on Shock-Wave/Boundary-Layer Interaction
Panel Aeroelastic Hysteresis Induced by Shock-Reflection Transition
Supersonic Retropropulsion Experimental Results from NASA Ames Foot Supersonic Wind Tunnel
Effects of Jet Temperature on Broadband Shock-Associated Noise
Correlation of Flowfield and Acoustic field Measurements in High-Speed Jets
Upstream Influence in Shock Wave/Transitional Boundary Layer Interactions at Mach 1.8
Flow Control of Swept Shock-Wave/Boundary-Layer Interaction Using Plasma Actuators
Supersonic Turbulent Boundary-Layer Separation Control Using a Morphing Surface
Plate-Angle Effects on Acoustic Waves from Supersonic Jets Impinging on Inclined Plates
Uncertainty and Sensitivity Analysis of Bleed Modeling in Shock/Turbulent Interactions
Identifying the Self-Sustaining Mechanisms of Transonic Airfoil Buffet with Resolvent Analysis
Detonation Initiation in a Tube via Imploding Toroidal Shock Waves
Wave Loading on Vertical Sheet-Pile Groins and Jetties
Investigation of a High-Mach-Number Overexpanded Jet Using Large-Eddy Simulation
Aeroacoustics of Three-Stream High-Speed Jets from Coaxial and Asymmetric Nozzles
Sound Produced by Large Area-Ratio Nozzles During Fixed and Transient Operations
Ghost Fluid Method for Strong Shock Interactions Part 1: Fluid-Fluid Interfaces
Rotating Detonation Wave Direction and the Influence of Nozzle Guide Vane Inclination
Propagation Analysis Using sBOOM for the Third AIAA Sonic Boom Prediction Workshop
Numerical Research of Spontaneous Condensation of Boron Oxide Vapor in Flat Nozzles
Links Between Steepened Mach Waves and Coherent Structures for a Supersonic Jet
A Coupled Inviscid–Viscous Airfoil Analysis Solver, Revisited
Unsteady Supersonic Flow for a Plate Undergoing Three-Stage Sinking Motion
Control of Fin Shock Induced Flow Separation Using Vortex Generators
Nonequilibrium Flows Revisited with a Generalized Chapman–Enskog Procedure