Aeroelasticity and Fuel Slosh!
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1 Aeroelasticity and Fuel Slosh! Robert Stengel, Aircraft Flight Dynamics! MAE 331, 2014" Aerodynamic effects of bending and torsion" Modifications to aerodynamic coefficients" Dynamic coupling" Fuel shift and sloshing dynamics" Flight Dynamics! , , ! Airplane Stability and Control! Chapter 19! Copyright 2014 by Robert Stengel. All rights reserved. For educational use only.! 1! The Elastic Airplane! Chapter 19, Airplane Stability and Control, Abzug and Larrabee! What are the principal subject and scope of the chapter?" What technical ideas are needed to understand the chapter?" During what time period did the events covered in the chapter take place?" What are the three main "takeaway" points or conclusions from the reading?" What are the three most surprising or remarkable facts that you found in the reading?" 2!
2 One-Dimensional Model of Aeroelasticity" 3! Republic P-47! Thunderbolt! Reduced Aileron Effect Due to Aeroelasticity" Wing torsion reduces aileron effect with increasing dynamic pressure" Rolling Criterion,! pb/2v! pb/2v elastic / pb/2v rigid! 4!
3 Aeroelastic Aileron Effect of Boeing Supersonic Transport Concept" Elastic-to- Rigid Ratio! Mach Number! 5! Quasi-Static Aeroelastic Model of Aircraft Dynamics: Residualization" IF elastic modes are fast compared to rigid modes and are stable" " #!!x aircraft 0 & ( F aircraft F elastic elastic F # aircraft aircraft F elastic & #!x aircraft!x elastic & + # G aircraft G elastic % &!u aircraft Residualization reduces aeroelastic model order to rigid-body model order"!!x a = F a!x a " F e a F e "1 = F a!x a + G a!u a # F e a!x a + G e!u a % & + G a!u a 6!
4 Primary Longitudinal Aeroelastic Mode Shapes" Fuselage Bending! Wing Bending! Wing Torsion! 7! Aeroelastic Model of Aircraft Dynamics" Coupled model of rigid-body and elastic dynamics" " #!!x aircraft!!x elastic & = F aircraft F elastic elastic F # aircraft aircraft F elastic & #!x aircraft!x elastic % & + " # G aircraft G elastic % &!u aircraft 8!
5 Effect of Increasing Coupling of Single Aeroelastic Mode with Short Period Roots " Fuselage Bending! Elastic Mode! Wing Torsion! Short Period! Mode! Wing Bending! Fuselage Bending! and Wing Torsion! Flight Dynamics, 5.6! 9! Effects of Fuselage Aeroelasticity on Lateral-Directional Response to Rudder Step Input" Flight Dynamics, 6.6! 10!
6 Aeroelastic Oscillations" 11! Aeroelastic Problems of the Lockheed Electra" Prop-whirl flutter, 2 fatal accidents ( ) " Structural modifications made; aircraft remained in service until 1992" Predecessor of US Navy Orion P-3, still in service" 12!
7 Centerline station! 14! Two-Dimensional Model of Aeroelastic Airplane" 13! Longitudinal Structural Modes of Boeing Supersonic Transport Concept" Boeing ! Normalized Deflection!
8 B-1 Canards for Ride Control" Elastic modes cause severe, high-g cockpit vibration during lowaltitude, high-speed flight" Active canard surfaces reduce amplitude of the oscillations" 15! Ultra-Light Aircraft" Extreme aeroelasticity" AeroVironment Pathfinder, Centurion, PathfinderPlus (solar-electric)" Helios in turbulence" 16!
9 The Last Flight of Helios" June 6, 2003 " 2,320 lb., 247-ft wingspan, 72 control surfaces, differential thrust" Change in weight distribution " 40-ft tip deflection" Divergent pitch oscillations, doubling every 8 seconds" Airspeed > 2.5 x limit" 17! Fuel Shift and Slosh! 18!
10 Fuel Shift" Problem with partially filled fuel tank" Single wing tank from tip to tip (A4D)" Slow, quasi-static shift of fuel c. m." Rudder step throws fuel to one side, producing a strong rolling moment" Abzug & Larrabee! 19! Fuel Shift"!! NTSB/AAB-04/01"!! Loss of Control and Impact with Terrain,"!! Canadair Challenger CL-604 Flight Test Airplane, C-FTBZ,"!! Wichita, Kansas, October 10, 2000" Flight Data Recording! Normal Acceleration! Angle of Attack! Pitch Angle! Elevator Angle!!! Probable Cause"!! Aft c.m. test"!! Pilot s excessive takeoff rotation"!! Rearward shift of c.m. due to fuel migration"!! Pitchup and subsequent stall"!! Inadequate test planning" IAS! Altitude! 20!
11 Dynamic oscillation of fuel center of mass, wave motion at the fuels surface" Pendulum and spherical-tank analogies" Problem is greatest when tank is half-full" Fuel Slosh" Fore-aft slosh in wing-tip tanks coupled with the short period mode (P-80)" Fuselage tank forward of the aircrafts center of mass (A4D)"! Yawing motion excites oscillatory slosh that couples with Dutch roll mode" Abzug & Larrabee! 21! Fuel Slosh" Solution: Fuel-tank baffles"! Slow down fuel motion"! Force resonances to higher frequencies due to smaller cavities"! Wing internal bracing may act as baffle" 22!
12 Problems of Fuel Slosh and Aeroelasticity" Coupling of non-rigid dynamic modes with rigid-body modes" Resonant response"! Dynamically coupled modes of motion with similar frequencies"! With light damping, oscillatory amplitudes may become large" " #!!x aircraft!!x elastic!!x slosh = & # F aircraft elastic F aircraft slosh F aircraft aircraft F elastic F elastic slosh F elastic aircraft F slosh elastic F slosh F slosh Coupling between longitudinal and lateral-directional effects" Nonlinear aerodynamics" Exacerbated by floating control surfaces, high hinge moments, and high aerodynamic angles! & #!x aircraft!x elastic!x slosh % + G!u & 23! Next Time:! High Speed and Altitude! Flight Dynamics! ! Airplane Stability and Control! Chapter 11! 24!
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