A Variational Formulation of the Compressible Throughflow Problem

Abstract

A variational formulation of the compressible throughflow flow problem is developed. The method is suitable for the calculation of throughflow fields in which large rotational effects, large compressibility effects and large variations in hub and tip radii may exist. The formulation requires the absence of viscous forces between blade rows, though the effects of losses within the blade rows may be included through the variation of entropy across streamsurfaces. The meridional Mach number is restricted to be less than unity, though the complete flow Mach number may be much in excess of unity. The variational formulation represents a complete statement of the problem in that the boundary conditions, far upstream and far downstream conditions, and matching conditions at all actuator discs are all natural conditions of the variational formulation.

Open PDF

Document Details

Document Type
Technical Report
Publication Date
Aug 01, 1974
Accession Number
ADA007979

Entities

People

  • Gordon C. Oates
  • Graham F. Carey

Organizations

  • University of Washington

Tags

Communities of Interest

  • Air Platforms
  • Materials and Manufacturing Processes

DTIC Thesaurus Topics

  • Actuators
  • Air Force
  • Angular Momentum
  • Boundaries
  • Computational Fluid Dynamics
  • Computational Science
  • Computer Programs
  • Differential Equations
  • Finite Element Analysis
  • Flow
  • Flow Fields
  • Geometry
  • Mach Number
  • Mechanical Properties
  • Nonlinear Systems
  • Numerical Analysis
  • Turbines

Fields of Study

  • Physics

Readers

  • Aerodynamics.
  • Fluid Dynamics.