One-Dimensional Compressible Flow in Variable Area Duct with Heat Addition (Preprint)

Abstract

One-dimensional compressible flows of calorically perfect gases in which only a single driving potential is present are called simple flows. Because Mach number and property relations for simple flows can be expressed in closed form, such flows are usually treated individually. Most introductory compressible flow courses and most compressible flow textbooks discuss three types of simple flows: isentropic flow in a variable area duct, the heat addition (or rejection) flow in constant area duct (Rayleigh flow), and adiabatic flow in a constant area duct with gas-wall-surface friction (Fanno flow). In the present paper we consider a case of two driving potentials: heat addition and variable area duct. Therefore, the obtained governing ordinary differential equations cannot be solved analytically, as in the case of simple flows, but they can be easily solved numerically. This research has been inspired by recent papers, where the authors discussed the thrust augmentation of solid rocket motors by heating the alumina particles in the exhaust of the motor by a microwave beam generated by a ground-based microwave generation facility. Thus, the equations obtained in the paper can be used, for example, as benchmarks for numerical investigation of gas flows in a nozzle heated by an external heating source.

Open PDF

Document Details

Document Type
Technical Report
Publication Date
Jun 25, 2010
Accession Number
ADA524450

Entities

People

  • Leonid Pekker

Tags

Communities of Interest

  • Energy and Power Technologies
  • Weapons Technologies

DTIC Thesaurus Topics

  • Air Force Research Laboratories
  • Compressible Flow
  • Demographic Cohorts
  • Differential Equations
  • Equations
  • Flow
  • Fluid Flow
  • Gas Flow
  • Ground Based
  • Heat Transfer
  • Mach Number
  • Microwave Beams
  • Microwaves
  • Rocket Engines
  • Rockets
  • Thrust
  • Thrust Augmentation

Readers

  • Combustion and Flow Dynamics.
  • Fluid Mechanics and Fluid Dynamics.
  • Theoretical Analysis.