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title: AIAA international space planes and hypersonic systems and technologies conference
Viscous Drag Reduction in a Mach 12 Scramjet Engine
Virtual Experiment for Optimization of Fuel Distribution in a Scramjet Engine (AIAA 2015-3598)
Virtual Experiment for Optimization of Fuel Distribution in a Scramjet Engine
Velocity Profile Modification in High-Speed Flows
Velocity measurement in a dual-mode supersonic combustor using particle image velocimetry
Velocity Field in Secondary Combustor of Ejector-Jet
VELOCITY FIELD IN SECONDARY COMBUSTOR OF EJECTOR-JET
VeLChYD - Very Low Cost Hypersonic Demonstrator for a Complete Orbital Reentry Mission
Vehicle evaluations for tether-assisted launch to orbit
Vehicle concepts for an ejector ramjet combined cycle engine
Vehicle and Mission Design of a Future Small Payload Launcher (AIAA 2017-2224)
Van Leer flux-splitting algorithm for nonequilibrium flows including vibrational relaxation
Validity of an Assumed PDF Combustion Model For SCRAMJET Applications
Validity of an Assumed-PDF Combustion Model For SCRAMJET Applications
Validation of Tools to Accelerate High-Speed CFD Simulations Using OpenFOAM (AIAA 2015-3566)
Validation of Tools to Accelerate High-Speed CFD Simulations Using OpenFOAM
Validation of the IXV Mission Analysis and Flight Mechanics Design
VALIDATION OF THE IXV MISSION ANALYSIS AND FLIGHT MECHANICS DESIGN
Validation of PIV measurements using Supersonic Turbulent Boundary Layer
VALIDATION OF PIV MEASUREMENTS USING SUPERSONIC TURBULENT BOUNDARY LAYER
Validation of global aeropropulsive characteristics of integrated configurations
Validation of Global Aeropropulsive Characteristics of Integrated Configurations