Accession Number:

ADA162351

Title:

Acta Aerodynamics Sinica (Selected Articles),

Descriptive Note:

Corporate Author:

FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OH

Report Date:

1985-11-22

Pagination or Media Count:

95.0

Abstract:

Contents A Fast Algorithm of the Finite Difference Method for the Computation of the Transonic flow Past an Arbitrary Air foil with the Conservation of the Full Potential Equation A Mixed Finite Difference Analysis of the Internal and External Transonic Flow Fields of Center Cone Inlet Numerical Method for Viscous Shock-layer near the Stagnation Line of a Blunt Body The Perfection and Application of the Flutter Subcritical Response Analysis Calculation of Octagonal Wall Interference Factor Using Conformal Mapping and Cryogenic High Reynolds Number Transonic Wind Tunnel with Pre-cooled and Restricted Flow.

Subject Categories:

  • Theoretical Mathematics
  • Fluid Mechanics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE