Accession Number:

AD0745103

Title:

Simulation of the Induced Flow through a Rotor in Descending Flight.

Descriptive Note:

Research and development technical rept.,

Corporate Author:

ARMY ELECTRONICS COMMAND FORT MONMOUTH N J

Personal Author(s):

Report Date:

1972-06-01

Pagination or Media Count:

31.0

Abstract:

The report outlines an emperical modification to classified momentum theory for the modeling of the induced flow through a rotor in descending flight. Consideration is also given to the computational stability of the procedure with emphasis upon the real-time representation of the system within a digital computer. Author

Subject Categories:

  • Fluid Mechanics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE