Accession Number:

ADA025186

Title:

Users Manual: Supersonic Unsteady Cascade Program. Volume II.

Descriptive Note:

Final rept. 22 Apr-22 Dec 75,

Corporate Author:

AERONAUTICAL RESEARCH ASSOCIATES OF PRINCETON INC N J

Personal Author(s):

Report Date:

1975-12-01

Pagination or Media Count:

39.0

Abstract:

This report is a users manual for a linearized unsteady supersonic cascade program. The basic theory is summarized in Section II together with a brief description of the numerical algorithm. A detailed description of how to use the program is given in Section III. The program can be used to calculate unsteady lift and moment coefficients on a supersonic finite two-dimensional cascade in a wind tunnel or free stream. Individual blades are excited in translation or rotation and the lift and moment coefficients are calculated on all other blades. An optional modified Kutta condition is included in the program. The detailed underlying theory is included in a companion technical report Analysis of Supersonic Unsteady Cascades with the Method of Characteristics, AFFDL-TR-159, Volume I, December 1975. Author

Subject Categories:

  • Computer Programming and Software
  • Fluid Mechanics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE