دورية أكاديمية
Static Stability and Axial Force Tests of the Holloman Monorail Rocket Sled at Mach Numbers 8 and 10
| العنوان: | Static Stability and Axial Force Tests of the Holloman Monorail Rocket Sled at Mach Numbers 8 and 10 |
|---|---|
| المؤلفون: | Rhudy, R W, Corce, J D |
| المساهمون: | ARNOLD ENGINEERING DEVELOPMENT CENTER ARNOLD AFB TN |
| المصدر: | DTIC AND NTIS |
| سنة النشر: | 1976 |
| المجموعة: | Defense Technical Information Center: DTIC Technical Reports database |
| مصطلحات موضوعية: | Test Facilities, Equipment and Methods, AERODYNAMIC CHARACTERISTICS, ROCKET SLEDS, AERODYNAMIC FORCES, BOUNDARY LAYER, CANARD CONFIGURATIONS, FLOW VISUALIZATION, HYPERSONIC CHARACTERISTICS, HYPERSONIC WIND TUNNELS, INTERACTIONS, NOSE CONES, SHOCK WAVES, STATIC STABILITY, WIND TUNNEL MODELS, WIND TUNNEL TESTS, Monorail rocket sleds |
| الوصف: | Experimental static-stability and axial-force data are presented for several configurations of a 0.4-scale model of a monorail rocket sled at Mach numbers of 8 and 10. The test Reynolds numbers, based on maximum model length, were approximately 14.4 and 10.7 million, respectively. The models were tested in close proximity to a ground plane assembly which simulated the rail and trough of the Holloman AFB High-Speed Test Track. Results are presented to show the effects of configuration variables such as nose shape; vertical, forward, and aft canards; rocket booster chamber length; and forward and aft slipper wedges. ; Prepared in cooperation with ARO, Inc., Tullahoma, TN. Rept. no. ARO-VKF-TR-75-122. |
| نوع الوثيقة: | text |
| وصف الملف: | text/html |
| اللغة: | English |
| العلاقة: | http://www.dtic.mil/docs/citations/ADA021391Test |
| الإتاحة: | http://www.dtic.mil/docs/citations/ADA021391Test http://oai.dtic.mil/oai/oai?&verb=getRecord&metadataPrefix=html&identifier=ADA021391Test |
| حقوق: | Approved for public release; distribution is unlimited. |
| رقم الانضمام: | edsbas.8E52B2D0 |
| قاعدة البيانات: | BASE |
| الوصف غير متاح. |