K. A. Fiscko

Application of Split-Film Anemometer and Mini-Computer for Measurement in Turbulent Separated Flow

W. H. Wentz, D. C. Howe, K. A. Fiscko, 1979 .

Wind tunnel force and pressure tests of a 21% thick general aviation airfoil with 20% aileron, 25% slotted flap and 10% slot-lip spoiler

W. H. Wentz, K. A. Fiscko, 1979 .

Force and pressure tests of the GA(W)-1 airfoil with a 20% aileron and pressure tests with a 30% Fowler flap

W. H. Wentz, H. C. Seetharam, K. A. Fiscko, 1977 .