BLADE-RATE FORCE FLUCTUATIONS OF A PROPELLER IN NON-UNIFORM FLOW

When a propeller rotates in a non-uniform flow field, unsteady propeller forces are generated at blade-rate frequency and its harmonics. A method of calculating these forces based upon two-dimensional unsteady aerofoil theory is described. A listing of a FORTRAN program to carry out these calculations is provided, together with a numerical example, and information about using the program. It is believed that this technique is a satisfactory compromise, achieving adequate accuracy with minimal computing cost; its use is recommended as a regular design tool. (Author)

  • Corporate Authors:

    Admiralty Research Laboratory

    Teddington,   England 
  • Authors:
    • Murray, M T
    • Tubby, J E
  • Publication Date: 1973-6

Media Info

  • Pagination: 51 p.

Subject/Index Terms

Filing Info

  • Accession Number: 00053917
  • Record Type: Publication
  • Source Agency: National Technical Information Service
  • Report/Paper Numbers: ARL/M/P33A
  • Files: TRIS
  • Created Date: May 7 1974 12:00AM