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Volumn , Issue , 1999, Pages
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An improved wind tunnel configuration for the investigation of aerodynamic cross wind gust response
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Author keywords
[No Author keywords available]
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Indexed keywords
FIGHTER AIRCRAFT;
SIGNAL TO NOISE RATIO;
TESTING;
WIND TUNNELS;
EXPERIMENTAL MODELING;
IMPROVED TECHNIQUES;
MULTIPLE DATA SETS;
PASSENGER VEHICLES;
PHASE AVERAGING TECHNIQUES;
SURFACE PRESSURE MEASUREMENTS;
VEHICLE MODEL;
WORKING SECTION;
AERODYNAMIC CONFIGURATIONS;
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EID: 85072418503
PISSN: 01487191
EISSN: 26883627
Source Type: Journal
DOI: 10.4271/1999-01-0808 Document Type: Conference Paper |
Times cited : (27)
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References (7)
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