Scramjet Fuel Injection Array Optimization Utilizing Mixed Variable Pattern Search With Kriging Surrogates

Abstract

Fuel-air mixing analysis of scramjet aircraft is often performed through experimental research or computational fluid dynamics (cfd) algorithms. Design optimization with these approaches is often impossible under a limited budget due to their high cost per run. This investigation uses jetpen, a known inexpensive analysis tool, to build upon a previous case study of scramjet design optimization. Mixed Variable Pattern Search (mvps) is compared to evolutionary algorithms in the optimization of two scramjet designs. The first revisits the previously studied approach and compares the quality of mvps to prior results. The second applies mvps to a new scramjet design in support of the Hypersonic International Flight Research Experimentation (hifire). The results demonstrate the superiority of mvps over evolutionary algorithms and paves the way for design optimization with more expensive approaches.

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Document Details

Document Type
Technical Report
Publication Date
Mar 01, 2008
Accession Number
ADA500329

Entities

People

  • Bryan Sparkman

Organizations

  • Air Force Institute of Technology

Tags

Communities of Interest

  • Air Platforms
  • Weapons Technologies

DTIC Thesaurus Topics

  • Air Force
  • Algorithms
  • Boundary Layer
  • Combustion
  • Computational Fluid Dynamics
  • Computational Science
  • Computer Programs
  • Differential Equations
  • Dynamic Pressure
  • Evolutionary Algorithms
  • Fluid Dynamics
  • Genetic Algorithms
  • Heat Transfer
  • Reliability
  • Specific Heat
  • Supersonic Combustion Ramjet Engines
  • Three Dimensional

Fields of Study

  • Physics

Readers

  • Adaptive Control and Estimation with Uncertainty in Dynamic Systems.
  • Combustion and Flow Dynamics.
  • Distributed Systems and Data Platform Development

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Flow