An Improved Method for Calculating Supersonic Pressure Fields about Bodies of Revolution PDF Download

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An Improved Method for Calculating Supersonic Pressure Fields about Bodies of Revolution

An Improved Method for Calculating Supersonic Pressure Fields about Bodies of Revolution PDF Author: Robert J. Mack
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 44

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Book Description
Development of near-field method for determining supersonic flow properties about bodies of revolution.

An Improved Method for Calculating Supersonic Pressure Fields about Bodies of Revolution

An Improved Method for Calculating Supersonic Pressure Fields about Bodies of Revolution PDF Author: Robert J. Mack
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 44

Get Book Here

Book Description
Development of near-field method for determining supersonic flow properties about bodies of revolution.

An Improved Method for Calculating Supersonic Pressure Fields about Bodies of Revolution

An Improved Method for Calculating Supersonic Pressure Fields about Bodies of Revolution PDF Author: Robert J. Mack
Publisher:
ISBN:
Category :
Languages : en
Pages : 34

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Book Description

NASA Technical Note

NASA Technical Note PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 390

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An Example for the Practical Calculation of Supersonic Flow Fields Past Oscillating Bodies of Revolution by a Method Due to Sauer

An Example for the Practical Calculation of Supersonic Flow Fields Past Oscillating Bodies of Revolution by a Method Due to Sauer PDF Author: Johann Muench
Publisher:
ISBN:
Category :
Languages : en
Pages : 16

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NASA Technical Paper

NASA Technical Paper PDF Author:
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 84

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NASA Technical Memorandum

NASA Technical Memorandum PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 52

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A Method for Determining the Total Drag of a Pointed Body of Revolution in Supersonic Flow with Turbulent Boundary Layer

A Method for Determining the Total Drag of a Pointed Body of Revolution in Supersonic Flow with Turbulent Boundary Layer PDF Author: Charlie M. Jackson
Publisher:
ISBN:
Category : Boundary layer
Languages : en
Pages : 74

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A Study of Methods which Predict Supersonic Flow Fields from Body Geometry, Distance, and Mach Number

A Study of Methods which Predict Supersonic Flow Fields from Body Geometry, Distance, and Mach Number PDF Author: Robert J. Mack
Publisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 36

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Applied Mechanics Reviews

Applied Mechanics Reviews PDF Author:
Publisher:
ISBN:
Category : Mechanics, Applied
Languages : en
Pages : 300

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UTIAS Report

UTIAS Report PDF Author: University of Toronto. Institute for Aerospace Studies
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 372

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Book Description