Electronic Resource
Unsteady Pressure and Force Measurements Associated with Transonic Buffeting of a Two-Dimensional Supercritical Airfoil (Mesures de Pression et de Force Instationnaires dues au Buffeting Transsonique d'un Profil Aerodynamique Surcritique Bidimensionnel).
العنوان: | Unsteady Pressure and Force Measurements Associated with Transonic Buffeting of a Two-Dimensional Supercritical Airfoil (Mesures de Pression et de Force Instationnaires dues au Buffeting Transsonique d'un Profil Aerodynamique Surcritique Bidimensionnel). |
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المؤلفون: | NATIONAL AERONAUTICAL ESTABLISHMENT OTTAWA (ONTARIO), Lee,B H K, Ohman,L H |
المصدر: | DTIC AND NTIS |
بيانات النشر: | 1983-06 |
نوع الوثيقة: | Electronic Resource |
مستخلص: | Buffet characteristics of the BGK No. 1 shockless airfoil have been investigated. Fluctuating pressure measurements along the airfoil chord and unsteady force balance data have been obtained in various regions inside the buffet regime close to the onset boundary curve. The Mach number range where buffet intensity reaches high values is determined from balance measurements. The rms values of the fluctuating pressure show generally monotonic increase downstream of the shock to the trailing-edge in this speed range. Statistical data from pressure and normal force measurements have been processed and the appearance of distinct frequency peaks in the power spectral density curves has been detected. in French. |
مصطلحات الفهرس: | Fluid Mechanics, Supercritical wings, Airfoils, Aerodynamic characteristics, Buffeting, Unsteady flow, Pressure distribution, Pressure measurement, Boundary layer flow, Transonic flow, Downstream flow, Shockless airfoils, Transonic buffeting, Text |
URL: | |
الاتاحة: | Open access content. Open access content Availability: Document partially illegible. |
ملاحظة: | text/html English |
Other Numbers: | DTICE ADA133139 831563882 |
المصدر المساهم: | From OAIster®, provided by the OCLC Cooperative. |
رقم الانضمام: | edsoai.ocn831563882 |
قاعدة البيانات: | OAIster |
الوصف غير متاح. |