Electronic Resource
AN/SSQ-41A/53 SONODROP: Flocelerator/Decelerator Wind Tunnel Test Results
| العنوان: | AN/SSQ-41A/53 SONODROP: Flocelerator/Decelerator Wind Tunnel Test Results |
|---|---|
| المؤلفون: | NAVAL AIR DEVELOPMENT CENTER WARMINSTER PA AIR VEHICLE TECHNOLOGY DEPT, Gombos, E. R., Reed, E. A. |
| المصدر: | DTIC AND NTIS |
| بيانات النشر: | 1975-02-24 |
| نوع الوثيقة: | Electronic Resource |
| مستخلص: | The Naval Air Development Center has conducted an analysis of aerodynamic decelerators for A-size sonobuoys. To obtain pertinent aerodynamic information, particularly drag data on various decelerators and flocelerators needed for mathematical simulation and future design, the Glenn L. Martin Institute of Technology Low Speed Wind Tunnel at the University of Maryland was utilized. This report summarizes the testing effort involved and presents the data for application to the refinement of current A-size sonobuoys. |
| مصطلحات الفهرس: | Gliders and Parachutes, Acoustic Detection and Detectors, AIR DROP OPERATIONS, SONOBUOYS, DECELERATION, DEPLOYMENT, DROGUE PARACHUTES, WIND TUNNEL MODELS, PARACHUTES, DECELERATORS, FLOCELERATORS, AN/SSQ-41A/53, AN/SSQ-41, Text |
| URL: | |
| الاتاحة: | Open access content. Open access content Approved for public release; distribution is unlimited. |
| ملاحظة: | text/html English |
| Other Numbers: | DTICE ADA008560 832008213 |
| المصدر المساهم: | From OAIster®, provided by the OCLC Cooperative. |
| رقم الانضمام: | edsoai.ocn832008213 |
| قاعدة البيانات: | OAIster |
| الوصف غير متاح. |