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Cover image for Validation of the NPARC code for nozzle afterbody flows at transonic speeds

Validation of the NPARC code for nozzle afterbody flows at transonic speeds

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Joyner - Microforms B300 NAS 1.15:106971 ✔ Available
Cover image for Supersonic wind tunnel tests of a half-axisymmetric 12°-spike inlet to a rocket-based combined-cycle propulsion system

Supersonic wind tunnel tests of a half-axisymmetric 12°-spike inlet to a rocket-based combined-cycle propulsion system

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Cover image for The numerical analysis of a turbulent compressible jet

The numerical analysis of a turbulent compressible jet

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Cover image for Experimental and analytical studies of flow through a ventral and axial exhaust nozzle system for STOVL aircraft

Experimental and analytical studies of flow through a ventral and axial exhaust nozzle system for STOVL aircraft

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Joyner - Microforms B300 NAS 1.15:104364 ✔ Available
Cover image for Rocket-based combined cycle engine technology development

Rocket-based combined cycle engine technology development

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Joyner - Microforms B300 NAS 1.15:107274 ✔ Available
Cover image for A comparison of three Navier-Stokes solvers for exhaust nozzle flowfields

A comparison of three Navier-Stokes solvers for exhaust nozzle flowfields

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Joyner - Microforms B300 NAS 1.15:209184 ✔ Available
Cover image for Comparison of high-order and low-order methods for large-eddy simulation of a compressible shear layer

Comparison of high-order and low-order methods for large-eddy simulation of a compressible shear layer

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Cover image for Assessment of computational fluid dynamics (CFD) models for shock boundary-layer interaction

Assessment of computational fluid dynamics (CFD) models for shock boundary-layer interaction

  • 2011
  • Format: Electronic
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Cover image for Prediction of turbulent temperature fluctuations in hot jets

Prediction of turbulent temperature fluctuations in hot jets

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Cover image for Numerical analysis of the trailblazer inlet flowfield for hypersonic Mach numbers

Numerical analysis of the trailblazer inlet flowfield for hypersonic Mach numbers

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