Published January 9, 2012 | Version public
Book Section - Chapter

Feasibility of Non-Equilibrium Hypersonic Flow Measurements at the Small Particle Hypervelocity Impact Range

  • 1. ROR icon Purdue University West Lafayette
  • 2. ROR icon Spectral Energies (United States)
  • 3. ROR icon California Institute of Technology
  • 4. ROR icon Jet Propulsion Lab

Abstract

Currently used hypersonic flow models, such as high-enthalpy reaction and energy relaxation rates, are based on experiments conducted at relatively low flow enthalpies and are highly uncertain. This paper presents analysis of the feasibility of calibrating hypersonic flow parameters using free-flight experiments at the Small Particle Hypervelocity Range (SPHIR) at Caltech/JPL. Chemically reacting, nonequilibrium flows around a 2-mm diameter spherical projectile are modeled using the Direct Simulation Monte Carlo (DSMC) method. The flowfields generated by DSMC simulations are used to calculate emission spectra in order to determine the observable radiation in UV/vis spectral range. Bayesian calibration and generalized polynomial chaos expansion (gPCE) techniques are used to assess the sensitivity of observable flow properties to key reaction rates. These techniques are then used to predict how experimental resolution would affect the uncertainty in the calibrated parameters.

Additional Information

© 2012 by the authors. Published by the American Institute of Aeronautics and Astronautics, Inc., with permission.

Additional details

Identifiers

Eprint ID
98311
Resolver ID
CaltechAUTHORS:20190828-102318872

Dates

Created
2019-08-28
Created from EPrint's datestamp field
Updated
2021-11-16
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Caltech Custom Metadata

Caltech groups
GALCIT
Other Numbering System Name
AIAA Paper
Other Numbering System Identifier
2012-0596