Accession Number:

AD0752928

Title:

A Numerical Solution for an Unsteady Two-Dimensional Jet-Flapped Wing.

Descriptive Note:

Technical rept.,

Corporate Author:

PENNSYLVANIA STATE UNIV UNIVERSITY PARK DEPT OF AEROSPACE ENGINEERING

Personal Author(s):

Report Date:

1972-11-01

Pagination or Media Count:

80.0

Abstract:

A numerical solution of the two-dimensional jet-flapped airfoil utilizing discrete vortices to represent airfoil and jet vortex distributions is presented for two time-dependent cases. The first concerns an instantaneous deflection of the jet exit angle and the second case involves continuous oscillation of the jet angle. Author

Subject Categories:

  • Aerodynamics
  • VSTOL
  • Fluid Mechanics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE