Development of Direct-Measuring Skin-Friction Gauges for Hypersonic Flight Tests

Author:

Smith Theodore B.1,Schetz Joseph A.1,Bui Trong T.2

Affiliation:

1. Virginia Polytechnic Institute and State University, Blacksburg, Virginia 20461

2. NASA Dryden Flight Research Center, Edwards, California 93523

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Cited by 10 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献

1. A two component friction balance based on ultrathin fiber Bragg grating pairs;Optical Fiber Technology;2024-03

2. Three components strain-gauge type aircraft surface friction resistance sensor: Design, manufacturing, and calibration;Measurement;2023-08

3. Temperature Drifts of The Floating Element Wall Shear Stress Sensor with Capacitive Sensing;2019 20th International Conference on Solid-State Sensors, Actuators and Microsystems & Eurosensors XXXIII (TRANSDUCERS & EUROSENSORS XXXIII);2019-06

4. The Direct Measurement of Skin Friction in Shock Tunnel;30th International Symposium on Shock Waves 1;2017

5. Surface micromachined differential piezoelectric shear-stress sensors;Journal of Micromechanics and Microengineering;2016-10-28

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