دورية أكاديمية
DRAG AND PERFORMANCE CHARACTERISTICS OF FLEXIBLE AERODYNAMIC DECELERATORS IN THE WAKE OF BASIC AND MODIFIED ARAPAHO C TEST VEHICLE CONFIGURATIONS AT MACH NUMBERS FROM 2 TO 5
| العنوان: | DRAG AND PERFORMANCE CHARACTERISTICS OF FLEXIBLE AERODYNAMIC DECELERATORS IN THE WAKE OF BASIC AND MODIFIED ARAPAHO C TEST VEHICLE CONFIGURATIONS AT MACH NUMBERS FROM 2 TO 5 |
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| المؤلفون: | Myers, A W, Hahn, J S |
| المساهمون: | ARNOLD ENGINEERING DEVELOPMENT CENTER ARNOLD AFB TN |
| المصدر: | DTIC AND NTIS |
| سنة النشر: | 1967 |
| المجموعة: | Defense Technical Information Center: DTIC Technical Reports database |
| مصطلحات موضوعية: | Gliders and Parachutes, Atmospheric Physics, Guided Missile Dynam, Config & Cntrl Surfaces, ATMOSPHERE ENTRY, DECELERATION, DROGUE PARACHUTES, AXISYMMETRIC FLOW, CONFIGURATIONS, DEPLOYMENT, DRAG, HIGH ALTITUDE, INSTRUMENTATION, NOSE CONES, OSCILLATION, PERFORMANCE(ENGINEERING), PITOT TUBES, PRESSURE, STABILITY, STRUCTURAL COMPONENTS, TEST METHODS, WAKE, WIND TUNNEL MODELS, STRUTS |
| الوصف: | Tests were conducted in the 40-in supersonic tunnel of the von Karman Gas Dynamics Facility to investigate the drag and decelerator models deployed at various positions aft of double-strut mounted forebodies. Data were obtained at Mach numbers from 2 to 5 at dynamic pressures corresponding to pressure altitudes which ranged from 41,000 to 140,000 ft. Selected typical results are presented. ; Prepared in cooperation with ARO, Inc., Tullahoma, Tenn. |
| نوع الوثيقة: | text |
| وصف الملف: | text/html |
| اللغة: | English |
| العلاقة: | http://www.dtic.mil/docs/citations/AD0813808Test |
| الإتاحة: | http://www.dtic.mil/docs/citations/AD0813808Test http://oai.dtic.mil/oai/oai?&verb=getRecord&metadataPrefix=html&identifier=AD0813808Test |
| حقوق: | Approved for public release; distribution is unlimited. |
| رقم الانضمام: | edsbas.61FCB575 |
| قاعدة البيانات: | BASE |
| الوصف غير متاح. |