Parametric Study of Relaminarization of Turbulent Boundary Layers on Nozzle Walls

Parametric Study of Relaminarization of Turbulent Boundary Layers on Nozzle Walls PDF Author: J. P. Kreskovsky
Publisher:
ISBN:
Category : Laminar flow
Languages : en
Pages : 102

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Parametric Study of Relaminarization of Turbulent Boundary Layers on Nozzle Walls

Parametric Study of Relaminarization of Turbulent Boundary Layers on Nozzle Walls PDF Author: J. P. Kreskovsky
Publisher:
ISBN:
Category : Laminar flow
Languages : en
Pages : 102

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Parametric Study of Relaminarization of Turbulent Boundary Layers on Nozzle Walls

Parametric Study of Relaminarization of Turbulent Boundary Layers on Nozzle Walls PDF Author: J. P. Kreskovsky
Publisher:
ISBN:
Category : Laminar flow
Languages : en
Pages : 100

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Scientific and Technical Aerospace Reports

Scientific and Technical Aerospace Reports PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1124

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Laminarization of a Turbulent Boundary Layer as Observed from Heat-transfer and Boundary-layer Measurements in Conical Nozzles

Laminarization of a Turbulent Boundary Layer as Observed from Heat-transfer and Boundary-layer Measurements in Conical Nozzles PDF Author: Donald R. Boldman
Publisher:
ISBN:
Category : Heat
Languages : en
Pages : 42

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Computational Fluid Mechanics and Heat Transfer

Computational Fluid Mechanics and Heat Transfer PDF Author: Dale Anderson
Publisher: Taylor & Francis
ISBN: 1466578300
Category : Science
Languages : en
Pages : 763

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Book Description
Thoroughly updated to include the latest developments in the field, this classic text on finite-difference and finite-volume computational methods maintains the fundamental concepts covered in the first edition. As an introductory text for advanced undergraduates and first-year graduate students, Computational Fluid Mechanics and Heat Transfer, Thi

Measurements of Upstream History Effects in Compressible Turbulent Boundary Layers

Measurements of Upstream History Effects in Compressible Turbulent Boundary Layers PDF Author: David F. Gates
Publisher:
ISBN:
Category : Supersonic nozzles
Languages : en
Pages : 124

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The report describes an experimental study of compressible turbulent boundary layers for which the upstream history was systematically varied. A series of experiments was conducted using both a supersonic half nozzle and a conventional flat plate for which the nozzle throat and flat plate leading edge can be temperature controlled. The supersonic nozzle provided a favorable upstream pressure gradient together with a controlled thermal history at the throat. The flat plate provided upstream temperature control with no pressure history. Velocity and temperature profile and heat-transfer measurements were made in a downstream region of zero-pressure-gradient and constant wall temperature. (Modified author abstract).

Laminarization of a Turbulent Boundary Layer in Nozzle Flow

Laminarization of a Turbulent Boundary Layer in Nozzle Flow PDF Author: L. H. Back
Publisher:
ISBN:
Category : Heat
Languages : en
Pages : 16

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Method for Predicting Compressible Turbulent Boundary Layers in Adverse Pressure Gradients

Method for Predicting Compressible Turbulent Boundary Layers in Adverse Pressure Gradients PDF Author: Shimer Zane Pinckney
Publisher:
ISBN:
Category : Boundary layer
Languages : en
Pages : 68

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Turbulence, Heat-transfer, and Boundary Layer Measurements in a Conical Nozzle with a Controlled Inlet Velocity Profile

Turbulence, Heat-transfer, and Boundary Layer Measurements in a Conical Nozzle with a Controlled Inlet Velocity Profile PDF Author: Donald R. Boldman
Publisher:
ISBN:
Category : Boundary layer
Languages : en
Pages : 44

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NASA Contractor Report

NASA Contractor Report PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 522

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