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Fixed Wing:

  • Smooth body separation Smooth body separation** Drag** Stability and control effectiveness** Maximum lift during approach/landing**
    • Drag
    • Stability and control effectiveness
    • Maximum lift during approach/landing

Fixed Wing:

    • 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 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

High Speed (Supersonic)

  • Shock/boundary layer interactions
  • Shock/expansion-jet plume interactions
  • Laminar to turbulent boundary layer flow transition
  • Sonic boom **
    • 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