Author:
Romblad Jonas,Ohno Duncan,Würz Werner,Krämer Ewald
Publisher
Springer International Publishing
Reference17 articles.
1. Airbus: Airbus’ “BLADE” laminar flow wing demonstrator makes first flight, Airbus press release 26.09.2017 (2017).
https://www.airbus.com/newsroom/press-releases/en/2017/09/airbus_-_blade_-laminar-flow-wing-demonstrator-makes-first-fligh.html
. Accessed 10 Aug 2018
2. Carta, F.O.: A comparison of the pitching and plunging response of an oscillating airfoil. NACA-CR-3172, National Aeronautics and Space Administration (1979)
3. Conte, S.: The numerical solution of linear boundary value problems. SIAM Rev. 8(3), 309–321 (1966)
4. Crouch, J.: Boundary-layer transition prediction for laminar flow control. In: 45th AIAA Fluid Dynamics Conference, p. 2472 (2015)
5. Franzoni, L.P., Elliott, C.M.: An innovative design of a probe-tube attachment for a 1/2-in. microphone. J. Acoust. Soc. Am. 104(5), 2903–2910 (1998)
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