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

doi 10.2514/6.2004-294
Full Text
Abstract

Available in full text

Date
Authors
Publisher

American Institute of Aeronautics and Astronautics

Related search

Recent Progress in Pressure-Sensitive Paint

Journal of the Visualization Society of Japan
2014English

Pressure-Sensitive Paint: Effect of Substrate

Sensors
InstrumentationInformation SystemsElectronic EngineeringBiochemistryAnalytical ChemistryMolecular Physics,ElectricalAtomicMedicineOptics
2011English

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

English

Application of Fast Pressure Sensitive Paint in Hypervelocity Flow

2011English

Pressure-Sensitive Paint Measurements of Hypersonic Flow in Shock Tunnel

Journal of the Japan Society for Aeronautical and Space Sciences
2003English

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

Journal of the Japan Society for Aeronautical and Space Sciences
1994English

Photodegradation Properties of Porous Pressure-Sensitive Paints

Journal of the Visualization Society of Japan
2002English

Pressure Sensitive Paint Measurements on 15% Scale Rotor Blades in Hover

2005English

A Linearized Euler Analysis of Unsteady Transonic Flows in Turbomachinery

Journal of Turbomachinery
Mechanical Engineering
1994English

Amanote Research

Note-taking for researchers

Follow Amanote

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

Privacy PolicyRefund Policy