Comments on NASA Langley Research on Transonic Unsteady Aerodynamics,

Abstract

Research is reported in an effort to fill the need for accurate unsteady transonic aerodynamics for use in flutter calculation. The paper describes five different approaches to the transonic unsteady flow problem. These methods each attempt to take into account the nonconstant Mach number characteristic of transonic flow, some more accurately than others. Viscous effects are not included.

Document Details

Document Type
Technical Report
Publication Date
Dec 01, 1973
Accession Number
AD0775066

Entities

People

  • Samuel R. Bland

Organizations

  • AGARD

Tags

DTIC Thesaurus Topics

  • Aerodynamics
  • Flow
  • Fluid Dynamics
  • Fluid Flow
  • Fluid Mechanics
  • Mach Number
  • Materials
  • Transonic Flow
  • Unsteady Aerodynamics
  • Unsteady Flow

Fields of Study

  • Physics

Readers

  • Aerodynamics.
  • Systems Analysis and Design