Accession Number:

ADA123982

Title:

Finite Difference Calculation of an Inviscid Transonic Flow over Oscillating Airfoils,

Descriptive Note:

Corporate Author:

ROYAL AIRCRAFT ESTABLISHMENT FARNBOROUGH (ENGLAND)

Personal Author(s):

Report Date:

1980-10-01

Pagination or Media Count:

45.0

Abstract:

Subject Categories:

  • Aircraft
  • Numerical Mathematics
  • Fluid Mechanics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE