A Method for Calculating Transient Surface Temperatures and Surface Heating Rates for High speed Aircraft

This book PDF is perfect for those who love Aerodynamic heating genre, written by Robert D. Quinn and published by Unknown which was released on 04 May 2024 with total hardcover pages 38. You could read this book directly on your devices with pdf, epub and kindle format, check detail and related A Method for Calculating Transient Surface Temperatures and Surface Heating Rates for High speed Aircraft books below.

A Method for Calculating Transient Surface Temperatures and Surface Heating Rates for High speed Aircraft
A Method for Calculating Transient Surface Temperatures and Surface Heating Rates for High speed Aircraft
Author : Robert D. Quinn
File Size : 49,7 Mb
Publisher : Unknown
Language : English
Release Date : 04 May 2024
ISBN : NASA:31769000450596
Pages : 38 pages
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A Method for Calculating Transient Surface Temperatures and Surface Heating Rates for High speed Aircraft by Robert D. Quinn Book PDF Summary

This report describes a method that can calculate transient aerodynamic heating and transient surface temperatures at supersonic and hypersonic speeds. This method can rapidly calculate temperature and heating rate time-histories for complete flight trajectories. Semi-empirical theories are used to calculate laminar and turbulent heat transfer coefficients and a procedure for estimating boundary-layer transition is included. Results from this method are compared with flight data from the X-15 research vehicle, YF-12 airplane, and the Space Shuttle Orbiter. These comparisons show that the calculated values are in good agreement with the measured flight data.

A Method for Calculating Transient Surface Temperatures and Surface Heating Rates for High speed Aircraft

A Method for Calculating Transient Surface Temperatures and Surface Heating Rates for High speed Aircraft by Robert D. Quinn

This report describes a method that can calculate transient aerodynamic heating and transient surface temperatures at supersonic and hypersonic speeds. This method can rapidly calculate temperature and heating rate time-histories for complete flight trajectories. Semi-empirical theories are used to calculate laminar and turbulent heat transfer coefficients and a procedure for

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A Method for Calculating Transient Surface Temperatures and Surface Heating Rates for High Speed Aircraft

A Method for Calculating Transient Surface Temperatures and Surface Heating Rates for High Speed Aircraft by National Aeronautics and Space Administration (NASA)

This report describes a method that can calculate transient aerodynamic heating and transient surface temperatures at supersonic and hypersonic speeds. This method can rapidly calculate temperature and heating rate time-histories for complete flight trajectories. Semi-empirical theories are used to calculate laminar and turbulent heat transfer coefficients and a procedure for

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Calculation of Surface Temperatures in Steady Supersonic Flight

Calculation of Surface Temperatures in Steady Supersonic Flight by George P. Wood

Surface temperatures were calculated for bodies in steady supersonic flight at Mach numbers from 2 to 10 and for altitudes from 50,000 and 200,000 feet and emissivities from 0 to 1. The importance of the effects of radiation and convection was determined. It was found, under the assumption of an isothermal atmosphere, that the gain of

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Structural Failure Analysis and Prediction Methods for Aerospace Vehicles and Structures by Sook-Ying Ho

This book deals with structural failure (induced by mechanical, aerodynamic, acoustic and aero-thermal, loads, etc.) of modern aerospace vehicles, in particular high-speed aircraft, solid propellant rocket systems and hypersonic flight vehicles, where structural integrity, failure prediction and service life assessment are particularly challenging, due to the increasingly more demanding mission

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The book addresses the overall integrated design aspects of a space transportation system involving several disciplines like propulsion, vehicle structures, aerodynamics, flight mechanics, navigation, guidance and control systems, stage auxiliary systems, thermal systems etc. and discusses the system approach for design, trade off analysis, system life cycle considerations, important aspects

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The measurement of heat-transfer data in a high-speed wind tunnel is considered in detail. The analysis is restricted to tests where transient temperature measurements are made by thermocouples attached to the back face of a thin-walled model. Methods of estimating the error in obtaining a heat-transfer coefficient due to extraneous

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The thermal analysis is presented of a portion of the external surface thermal protection system and load bearing structure of a hypersonic vehicle, whose mission consists of a climb-out to 100,000 feet, cruise at Mach 6, descent, and a final phase, termed turn around, which includes landing rollout, refueling and maintenance. Temperature-dependent

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A Review of High speed Convective Heat transfer Computation Methods

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Download or read online A Review of High speed Convective Heat transfer Computation Methods written by Michael E. Tauber, published by Unknown which was released on 1989. Get A Review of High speed Convective Heat transfer Computation Methods Books now! Available in PDF, ePub and Kindle.

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