Synonyme wurden verwendet für:
supersonic
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keywords:(supersonic)
Phugoid Motion Simulation of a Supersonic Transport Using Navier–Stokes Equations
Effects of Shock Waves on Shack–Hartmann Wavefront Sensor Data
Effect of Counterflowing Jet on Supersonic Slender-Body Configurations: A Numerical Study
Supersonic Boundary Layers with Periodic Surface Roughness
Investigation of Shear Layer Growth Influenced by Shock Waves in a Scramjet
Proper Orthogonal Decomposition Reduced-Order Model for Nonlinear Aeroelastic Oscillations
Effect of Low-Boom Waveform on Focus Boom Using Lossy Nonlinear Tricomi Analysis
Supersonic Retropropulsion Experimental Results from NASA Ames Foot Supersonic Wind Tunnel
Supersonic Retropropulsion Validation Experiment in the NASA Langley Unitary Plan Wind Tunnel
Estimation of Uncertainties for a Model Validation Experiment in a Wind Tunnel
Closed-Loop Control of Dynamic Oblique Shock with Arc Plasma
Flow Asymmetry in a Y-Shaped Diverterless Supersonic Inlet: A Novel Finding
Shock Wave/Boundary-Layer Interaction Control Using a Combination of Vortex Generators and Bleed
Nonlinear Characteristics of a Rectangular Cavity in Supersonic Flow
Mass Flux Sensing via Tunable Diode Laser Absorption of Water Vapor
Tail Flare vs Fins in the Design of a Subcaliber Projectile
Consistent Coupling of Compressibility Effects in Manifold-Based Models for Supersonic Combustion
Similarity and Key Parameters of Retropropulsion Assisted Deceleration in Hypersonic Wind Tunnels
Canonical Normal Shock Wave/Boundary-Layer Interaction Flows Relevant to External Compression Inlets
Reduction of Noise Generated by a Half-Open Weapons Bay
Review of "The Scramjet Engine, Processes and Characteristics"
Mach 3 Shock Wave Unsteadiness Alleviation Using a Negative Corona Discharge
Aerodynamic Characteristics of Circular and Noncircular Cross-Sectional Missile Configurations
Studies of Inlet Distortion in a Direct-Connect Axisymmetric Scramjet Isolator
Variable Noise Reduction Systems for a Notional Supersonic Business Jet
Roughness-Induced Transition in a Supersonic Boundary Layer
Effect of Interaction Strength on Unsteadiness in Shock-Wave-Induced Separations
Control of Cavity Oscillations in a Supersonic Flow by Microjet Injection
Aerodynamics of Lean Blowout in a Premixed Dual-Mode Scramjet
Penetration and Combustion Studies of Tandem Liquid Jets in Supersonic Crossflow
Simulations and Experiments of a Dual-Stream Low-Boom Supersonic Inlet
Examining Distributed Fueling Schemes Using Tandem Cavities in a Mach 8 Scramjet
Uncertainty and Sensitivity Analysis of Bleed Modeling in Shock/Turbulent Interactions
Supersonic Flutter Analysis Based on a Local Piston Theory
Freejet Experimental Investigation on Performance of Dual-Combustion Ramjet
Numerical Investigation of Gas Models for Retropropulsion Flows for Future Mars Missions
Ballistic Wave from Projectiles and Vehicles of Simple Geometry
Inlet Distortion Effects on Fuel Distribution and Ignition in Scramjet Cavity Flameholder
Flame Stabilization and Propagation in Dual-Mode Scramjet with Staged-Strut Injectors
Strut Injectors for Scramjets: Total Pressure Losses in Two Streamwise Vortex Interactions
Fluid and Combustion Dynamics in Axisymmetric and Perisymmetric Supersonic Combustion Flowpaths
Reduced-Order Comparison of Simulated and Measured Coalescing Mach Waves near Supersonic Jets
Experiments on High-Temperature Hypersonic Fluid–Structure Interaction with Plastic Deformation
Supersonic Exhaust from a Rotating Detonation Engine with Throatless Diverging Channel
Approximation of Off-Body Sonic-Boom Analysis for Low-Boom Conceptual Design