Transition Measurements on a 2-D Wing Boundary-Layer in Low-Subsonic Flight Test.
نویسندگان
چکیده
منابع مشابه
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متن کامل2.5. Measurements in a Two-Dimensional Boundary Layer and a Wing-Body Junction Flow
2.4. Pressure Transducer The Endevco model 8507-C2 pressure transducer (figure 10) was used for the present measurements. It is a high sensitivity piezoresistive, circular-deflection-type, pressure transducer that has a nominally flat frequency response from 0-70 kHz with a rated sensitivity of 130 mV/psi and a full scale output of 300 mV. The transducer contains an active four-arm strain gage ...
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ژورنال
عنوان ژورنال: JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES
سال: 2002
ISSN: 1344-6460
DOI: 10.2322/jjsass.50.380