Measurement of Aerodynamic Heating Rates Using Temperature-Sensitive-Paint.

Journal of the Japan Society for Aeronautical and Space Sciences
doi 10.2322/jjsass1969.42.154
Full Text
Abstract

Available in full text

Date
Authors
Publisher

Japan Society for Aeronautical and Space Sciences

Related search

Improved Pressure Sensitive Paint Measurement Using Natural Feature Tracking and Piecewise Linear Resection

English

Temperature and Velocity Measurement Using Temperature Sensitive Particles(Fluids Engineering)

Nihon Kikai Gakkai Ronbunshu, B Hen/Transactions of the Japan Society of Mechanical Engineers, Part B
Condensed Matter PhysicsMechanical Engineering
2009English

Porous Pressure-Sensitive Paint for Measurement of Unsteady Pressures in Turbomachinery

2004English

Note on Aerodynamic Heating

Quarterly of Applied Mathematics
Applied Mathematics
1951English

Hypersonic Aerodynamic Heating Prediction Using Weighted Essentially Nonoscillatory Schemes

Journal of Spacecraft and Rockets
SpacePlanetary ScienceAerospace Engineering
2003English

Pressure-Sensitive Paint: Effect of Substrate

Sensors
InstrumentationInformation SystemsElectronic EngineeringBiochemistryAnalytical ChemistryMolecular Physics,ElectricalAtomicMedicineOptics
2011English

Dynamic Distributed Measurement of Temperature Changes Using Phase-Sensitive OTDR With Chirped Pulses

2016English

Binary Pressure-Sensitive Paint Measurements Using Miniaturised, Colour, Machine Vision Cameras

Measurement Science and Technology
InstrumentationEngineeringApplied Mathematics
2018English

Recent Progress in Pressure-Sensitive Paint

Journal of the Visualization Society of Japan
2014English

Amanote Research

Note-taking for researchers

Follow Amanote

© 2024 Amaplex Software S.P.R.L. All rights reserved.

Privacy PolicyRefund Policy