دورية أكاديمية
LOCAL AERODYNAMIC PARAMETERS FOR SUPERSONIC AND HYPERSONIC FLUTTER ANALYSES
| العنوان: | LOCAL AERODYNAMIC PARAMETERS FOR SUPERSONIC AND HYPERSONIC FLUTTER ANALYSES |
|---|---|
| المؤلفون: | Olsen, James J |
| المساهمون: | AIR FORCE FLIGHT DYNAMICS LAB WRIGHT-PATTERSON AFB OH |
| المصدر: | DTIC AND NTIS |
| سنة النشر: | 1965 |
| المجموعة: | Defense Technical Information Center: DTIC Technical Reports database |
| مصطلحات موضوعية: | Fluid Mechanics, Mechanics, FLUTTER, HYPERSONIC FLOW, SUPERSONIC FLOW, AERODYNAMIC CHARACTERISTICS, AERODYNAMIC CONFIGURATIONS, MATHEMATICAL ANALYSIS, NOSE CONES, PANELS, SHOCK WAVES |
| الوصف: | The report presents the results of an analysis to determine how certain aerodynamic flutter parameters are changed from their free stream values by the existence of supersonic and hypersonic nose shock waves and expansions. The results indicate that nose shock waves and expansions can create a new set of 'free stream' conditions for flutter analyses. These new free stream conditions can be sufficiently different from the undisturbed 'free stream' condition to warrant their detailed analyses in the supersonic and hypersonic vehicle. |
| نوع الوثيقة: | text |
| وصف الملف: | text/html |
| اللغة: | English |
| العلاقة: | http://www.dtic.mil/docs/citations/AD0626928Test |
| الإتاحة: | http://www.dtic.mil/docs/citations/AD0626928Test http://oai.dtic.mil/oai/oai?&verb=getRecord&metadataPrefix=html&identifier=AD0626928Test |
| حقوق: | Approved for public release; distribution is unlimited. |
| رقم الانضمام: | edsbas.187C5652 |
| قاعدة البيانات: | BASE |
| الوصف غير متاح. |