Synonyme wurden verwendet für:
Waves
Suche ohne Synonyme:
keywords:(Mach Waves)
Parametric Cycle Analysis of an Ideal Pulse Detonation Engine
Hypersonic Transitional Shock-Wave–Boundary-Layer Interaction on a Flat Plate
Vortex Generators for Corner Separation Caused by Shock-Wave/Boundary-Layer Interactions
Shape Optimization of Vortex Generators to Control Mack Mode Amplification
Stabilization of a Mach 5.92 Boundary Layer by Two-Dimensional Finite-Height Roughness
Skylon Aerospace Plane and Its Aerodynamics and Plumes
Numerical Analysis of Ignition Overpressure Effect on H-IIB Launch Vehicle
Comparison of Shock/Cooling-Film Interaction for Cooled and Isoenergetic Injection
A Novel Reduced-Order Model for Predicting Compressible Cavity Flows
Toward a Comprehensive Model of Jet Noise Using an Acoustic Analogy
Buzz Cycle Description in an Axisymmetric Mixed-Compression Air Intake
A Near-Field Approach to the Sonic Boom Problem
Design of Control-Assisted Transonic Pressure Recovery Profiles Using Vortex Generators
Design of Low-Speed Slotted, Natural-Laminar-Flow Airfoil Reproducing Transonic Behaviors
High-Fidelity Simulations of Pressure-Gain Combustion Devices Based on Detonations
Thermal Performance of Transonic Cooled Tips in a Turbine Cascade
Experimental Study of Boundary-Layer Response to Laser-Generated Disturbances at Mach 6
Numerical Investigation of Transitional Shock-Wave/Boundary-Layer Interaction in Supersonic Regime
Simulation of Laser-Induced Plasma Ignition in a Hypersonic Crossflow
Shock-Induced Separation and Control in a 4.32-Aspect-Ratio Test Section
Investigation of Shear Layer Growth Influenced by Shock Waves in a Scramjet
Direct Visualization of Shock Waves in Supersonic Space Shuttle Flight
Wedge-Induced Oblique Detonations with Small Heat Release
Numerical Error in the Turbulence Model Applied to Eddy-Viscous Shock Waves
Effect of Nozzle–Plate Distance on Acoustic Phenomena from Supersonic Impinging Jet
Aerothermal Performance of Different Tips in Transonic Turbine Cascade with End-Wall Motion
Aeroacoustics of a Planar Multistream Supersonic Nozzle with Aft Deck and Sidewalls
Performance and Energy Expenditure of Coflow Jet Airfoil with Variation of Mach Number
Characterizing Streamwise Development of Surface Roughness Effects on a Supersonic Boundary Layer
Effect of Microramps on Separated Swept Shock Wave–Boundary-Layer Interactions
Shock-Wave Patterns on a Cranked-Wing Configuration
Characterization of Turbulent Supersonic Flow over a Backward-Facing Step
Modal Decomposition Analysis of Three-Dimensional Transonic Buffet Phenomenon on a Swept Wing
Wave-Packet Representation of Shock-Cell Noise for a Single Round Jet
Pressure-Gain Combustion Using Shock–Flame Interaction
Influence of External Flow on Plume Physics of Clustered Linear Aerospike Nozzles
Simulations of Cellular Detonation Interaction with Turbulent Flows
An Estimate of Turbulent Velocities in the Ocean
Propagation from moving sources in flows
Global Sensitivity Analysis and Uncertainty Quantification for a Hypersonic Shock Interaction Flow
Response of a Hypersonic Boundary Layer to Wall Blowing-Suction
Determination of Sun Angles for Observations of Shock Waves on a Transport Aircraft
Investigation of Surface Curvature Effects on Unseparated Fin Shock-Wave/Boundary-Layer Interactions