Prediction of unsteady aerodynamic loadings caused by trailing edge control surface motions in subsonic compressible flow: analysis and results
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Aerodynamic airfoil angle of attack Aspect Ratio asymptotic expansion boundary conditions Chordwise Downwash Distribution chordwise integral Chordwise Pressure Distributions collocation stations computer program continuous downwash distributions control points control surface configurations control surface hingeline control surface motions coordinate derivative dipole discontinuous downwash distributions downwash chord downwash discontinuities downwash distribution obtained Downwash Distribution Resulting downwash sheets downwash station edge control surfaces equation 19 experimental pressure finite flap deflection flow formulated hinge moments inboard integral of equation integrand kernel function kinematic distribution lifting surface linear loadings caused located logarithmic singularity Mach number mathematical downwash mode shape NACA non-singular nondimensional normalwash open gap Phase Angles planform definition planform discontinuities preferred solution process pressure function pressure loading functions quadrature formulas reference regions sealed gap sectional generalized forces semispan shown in figure spanwise loadings Subsonic subtracting symmetrical Taylor series theoretical and experimental theoretical pressure distributions tions trailing edge control velocity WADC wing wing-control surface