Accession Number:

ADA951986

Title:

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

Descriptive Note:

Corporate Author:

PRINCETON UNIV N J JAMES FORRESTAL RESEARCH CENTER

Personal Author(s):

Report Date:

1947-10-05

Pagination or Media Count:

18.0

Abstract:

Subject Categories:

  • Aircraft
  • Numerical Mathematics
  • Fluid Mechanics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE