Flow Visualisation Over the Low Sweep Unmanned Combat Aerial Vehicle (UCAV) Configuration
Author:
Publisher
Springer Nature Singapore
Link
https://link.springer.com/content/pdf/10.1007/978-981-19-3923-5_2
Reference15 articles.
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3. Loeser, T., Vicroy, D., Schuette, A.: SACCON static wind tunnel tests at DNW-NWB and 14x22 NASA LaRC. In: 28th AIAA Applied Aerodynamics Conference, p. 4393 (2010)
4. Wisnoe, W., Nasir, R.E., Ramly, R., Kuntjoro, W., Muhammad, F.: Aerodynamic of uitm’s blended-wing-body unmanned aerial vehicle baseline-II equipped with one central vertical rudder. Jurnal Teknologi 75(8), 95–99 (2015)
5. Gursul, I., Gordnier, R., Visbal, M.: Unsteady aerodynamics of nonslender delta wings. Prog. Aerosp. Sci. 41(7), 515–557 (2005)
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