Accession Number:

ADA426598

Title:

A Complete Rotor Wake Model in State Space

Descriptive Note:

Final rept. 1 Aug 2001-31 Jul 2004

Corporate Author:

WASHINGTON UNIV ST LOUIS MO

Personal Author(s):

Report Date:

2004-09-01

Pagination or Media Count:

25.0

Abstract:

This research deals with the development of a finite-state inflow theory that will be able to predict all three components of flow both on and off of the rotor disk. The theory will be of a velocity potential expanded in hierarchical degrees of freedom.

Subject Categories:

  • Helicopters
  • Fluid Mechanics
  • Theoretical Mathematics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE