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An Experimental Study on the Aerodynamic Characteristics of a Stealth Configuration
- Source :
- Journal of the Korean Society for Aeronautical & Space Sciences. 36:962-968
- Publication Year :
- 2008
- Publisher :
- The Korean Society for Aeronautical & Space Sciences, 2008.
-
Abstract
- An experimental study of the aerodynamic characteristics of a stealth configuration, the test techniques developed for the testing in the Low Speed Wind Tunnel of Agency for Defense Development(ADD-LSWT), and the lessons learned have been presented. The main objectives of this test are to determine the aerodynamic characteristics of a stealth configuration and to measure the flow field characteristics with a 5-hole pressure probe. The test results are discussed and the effect of the leading edge shape on the aerodynamic characteristics is also given.
Details
- ISSN :
- 12251348
- Volume :
- 36
- Database :
- OpenAIRE
- Journal :
- Journal of the Korean Society for Aeronautical & Space Sciences
- Accession number :
- edsair.doi...........4eb2545cf8de8c94e0e3c7a2502215f9