کد مقاله | کد نشریه | سال انتشار | مقاله انگلیسی | نسخه تمام متن |
---|---|---|---|---|
7153985 | 1462495 | 2017 | 5 صفحه PDF | دانلود رایگان |
عنوان انگلیسی مقاله ISI
Aerodynamic force and moment measurement of 10° half-angle cone in JF12 shock tunnel
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کلمات کلیدی
موضوعات مرتبط
مهندسی و علوم پایه
سایر رشته های مهندسی
مهندسی هوافضا
پیش نمایش صفحه اول مقاله
![عکس صفحه اول مقاله: Aerodynamic force and moment measurement of 10° half-angle cone in JF12 shock tunnel Aerodynamic force and moment measurement of 10° half-angle cone in JF12 shock tunnel](/preview/png/7153985.png)
چکیده انگلیسی
An aerodynamic force and moment measurement was conducted in JF12 long-test-duration detonation-driven shock tunnel of Institute of Mechanics, Chinese Academy of Sciences. The test duration of JF12 is 100-130 ms. The nominal Mach number is 7.0 and the exit diameter of the contoured nozzle is 2.5 m. The total enthalpy is 2.5 MJ/kg which duplicates the hypersonic flight conditions of Mach number 7.0 at 35 km altitude. The test model is the standard aerodynamic force model of 10° half-angle sharp cone. The length of the test model is 1500 mm and the weight is 57 kg. The aerodynamic forces were measured with a six-component strain balance. The angles of attack were set to be â5°, 0°, 5°, 10° and 14°, respectively. The experimental results show that in the 100-130 ms test duration, the signals of strain balance have 3-4 complete vibration cycles. So, the aerodynamic forces and moments can be obtained directly by averaging the signals of balance without acceleration compensation. The force measurement error of repeatability of JF12 is less than 2%. The aerodynamic force coefficients of JF12 are in good agreement with those of conventional hypersonic wind tunnels. For this test model at Mach number 7.0 and total enthalpy of 2.5 MJ/kg, the real-gas effects on aerodynamic force characteristics are not very evident.
ناشر
Database: Elsevier - ScienceDirect (ساینس دایرکت)
Journal: Chinese Journal of Aeronautics - Volume 30, Issue 3, June 2017, Pages 983-987
Journal: Chinese Journal of Aeronautics - Volume 30, Issue 3, June 2017, Pages 983-987
نویسندگان
Yunfeng LIU, Yunpeng WANG, Chaokai YUAN, Changtong LUO, Zonglin JIANG,