Page History

• • Transonic and low speed buffet
  • Boundary layer ingestion for tightly coupled airframe/engine installations
• Massive separation

• • Cavities

• • Extreme maneuvers

• • Blunt components

• • Dynamic stall
• Laminar to turbulent boundary layer flow transition

• • Natural and hybrid laminar flow control
• Viscous wake

• interactions and boundary layer confluence

• • Multi-element, high-lift flows
• Corner flows

• • Wing/body, wing/pylon, and pylon/nacelle juncture flows
• Reattachment
• Icing

• • Ice development and accretion

• • Performance impact
• Circulation and flow separation control

• • Active flow control

• • Powered lift
• Jet exhaust

• • Engine noise

• • Jet-flap interaction

• • Sonic fatigue
• Airframe noise

• • High-lift

• • Landing gear
• Vortical flows

• • Vortex generators/chines
• Wake hazard reduction and avoidance
• Wind tunnel to flight scaling

• • Reynolds number

• • Model characteristics: surface, brackets, aeroelastics

Rotary Wing:

• Flow separation

• • Bluff bodies

• • Hover download

• • Dynamic stall
• Vortical flow in rotor wakes

• • Wake persistence for large numbers of revolutions

• • Blade/vortex interactions
• Rotor structural dynamics/aerodynamics/controls interactions

• • Flexible/deformed rotor blade flows

• • Vibratory loads
• Rotor wake/fuselage interactions
• Flow interaction with ground

• • Ground wash

• • Brownout

• • Rotor/Airframe interaction with ground plane
• Acoustic loading
• Non-harmonic flow/rotor control
• Multi-rotor interactions (coaxial, etc.)
• Laminar to turbulent boundary layer transition flow
• Circulation and flow separation control

• • Active flow control
• Icing

• • Ice accretion

• • Ice shedding

• • Performance impact
• Wind tunnel to flight scaling

• • Reynolds number

• • Model characteristics

• • Shock wave coalescence

• • Propagation through atmospheric turbulence and/or wind shear
• MDAO of low boom / low drag design / high efficiency, low distortion inlet design
• Airframe/nacelle shock/viscous interactions
• Slender wing vortex flows
• Aero-propulsive-servo-elastic interactions for slender configurations
• Engine/jet nose acoustics
• Shock-induced flow separation in inlets and nozzles (un-start)
• Store separation

• • Booster staging

• • Weapon drop

High Speed (Hypersonic)

• Aerodynamic heating
• Interaction with ablative materials
• Radiative heating
• Boundary layer transition
• Low density effects at high altitudes
• Strong shock/boundary-layer and shock/shock interactions
• Finite-rate gas chemistry (with a complete set of chemical reactions)
• Ionization, non-equilibrium, and plasma flows during reentry
• Subsonic and supersonic combustion in dual-mode scramjets (possibly with liquid fuel injection)
• Flow separation

• • Inlets and nozzles (un-start)

• • Bluff bodies
• Jet interaction with freestream flow (augmentation factor)

Engine/Propulsion System

• Integrated propulsor/airframe flows
• Unsteady flows due to turbomachinery blade row interactions

• • Stage matching

• • Wake mixing

• • Compressor stability and rotating stall
• Secondary flows, including endwall and tip vortical structures
• Time-accurate coupled component interactions

• • Multi-row rotor-stator interactions

• • Main gaspath/secondary gaspath interactions

• • Combustor exhaust product/turbine interactions including hot streak migration
• Aerothermal cooling/mixing flows (e.g., film cooling)
• Rotational and curvature effects on flow turbulence for rotating turbomachinery
• Transitional flows over a wide range of Reynolds number, pressure gradient, and freestream turbulence
• Real gas thermodynamic models for high temperature flows with dissociation
• Reactive flows

• • Fuel spray modeling (two-phase flows, liquid fuel breakup, atomization, gaseous mixing)

• • Multi-regime combustion models

• • Emissions modeling
  • Vitiated flows
  • Combustion dynamics
• Near-field acoustic sources and propagation to the acoustic farfield
• Ice accretion
• Distributed (electric) propulsion