Accession Number : ADA951986

Title :   Application of Frequency Response Method to the Calculation of the Dynamic Stability Limits of Airplanes with Two Independent Autopilots,

Corporate Author : PRINCETON UNIV N J JAMES FORRESTAL RESEARCH CENTER

Personal Author(s) : Greenberg,Harry

Report Date : 05 OCT 1947

Pagination or Media Count : 18

Descriptors :   *Numerical methods and procedures, *Frequency response, *Aerodynamic stability, Computations, Automatic pilots, Control, Gears, Charts, Amplitude, Ratios, Phase, Angles, Ailerons, Aerial rudders, Yaw

Subject Categories : Aircraft
      Numerical Mathematics
      Fluid Mechanics

Distribution Statement : APPROVED FOR PUBLIC RELEASE