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2013•31st AIAA Applied Aerodynamics ConferenceRequires access

C-295 AEW aerodynamic design process: CFD, wind tunnel tests and flight tests

Angel Noel Castano Sanchez, Ernesto Rodriguez Cisneros, Emilio Javier Angel Blasco

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Abstract

ADB = Aerodynamic Data Base AEO = All Engine Operatives AEW = Airborne Early Warning b = Wing Span CD = Drag force coefficient Cf = Local skin friction coefficient CL = Lift Force Coeficient Cn = Yawing moment coefficient Cnβ = Yawing coefficient moment due to sideslip derivative Cnδr = Yawing coefficient moment due to rudder deflection derivative Cp = Pressure coefficient CYAWB = Cn C4IRS = Command, Control, Communications, Computers, Intelligence, Surveillance and Reconnaissance FT = Flight Test FI = Flight Idle LEI = Left Engine Inoperative PT = Total pressure PTinf = Total pressure of the free-stream Re = Reynolds number TC = Thrust coefficient WTT = Wind tunnel test Y = Lateral distance to aircraft symmetry plane  = Aircraft incidence β = Sideslip angle δF = Flap deflection angle

About this research paper

What this paper is about

ADB = Aerodynamic Data Base AEO = All Engine Operatives AEW = Airborne Early Warning b = Wing Span CD = Drag force coefficient Cf = Local skin friction coefficient CL = Lift Force Coeficient Cn = Yawing moment coefficient Cnβ = Yawing coefficient moment due to sideslip derivative Cnδr = Yawing coefficient moment due to rudder deflection derivative Cp = Pressure coefficient CYAWB = Cn C4IRS = Command, Control, Communications, Computers, Intelligence, Surveillance and Reconnaissance FT = Flight Test FI = Flight Idle LEI = Left Engine Inoperative PT = Total pressure PTinf = Total pressure of the free-stream Re = Reynolds number TC = Thrust coefficient WTT = Wind tunnel test Y = Lateral distance to aircraft symmetry plane  = Aircraft incidence β = Sideslip angle δF = Flap deflection angle

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Available abstract

ADB = Aerodynamic Data Base AEO = All Engine Operatives AEW = Airborne Early Warning b = Wing Span CD = Drag force coefficient Cf = Local skin friction coefficient CL = Lift Force Coeficient Cn = Yawing moment coefficient Cnβ = Yawing coefficient moment due to sideslip derivative Cnδr = Yawing coefficient moment due to rudder deflection derivative Cp = Pressure coefficient CYAWB = Cn C4IRS = Command, Control, Communications, Computers, Intelligence, Surveillance and Reconnaissance FT = Flight Test FI = Flight Idle LEI = Left Engine Inoperative PT = Total pressure PTinf = Total pressure of the free-stream Re = Reynolds number TC = Thrust coefficient WTT = Wind tunnel test Y = Lateral distance to aircraft symmetry plane  = Aircraft incidence β = Sideslip angle δF = Flap deflection angle

Key concepts: Aerodynamics, Computational fluid dynamics, Wind tunnel, Aerospace engineering, Marine engineering, Engineering, Process (computing), Aeronautics

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C-295 AEW aerodynamic design process: CFD, wind tunnel tests and flight tests — Research Paper | ScholarLens