Abstract
The development of the boundary layer in general and shock boundary layer interaction in particular essentially establish the flight performance of transonic transport aircraft at cruise and high-speed off-design conditions. Consequently, employing shock and boundary layer control can be assumed to have a large potential for improving flight performance in terms of cruise drag, hence speed and / or fuel consumption, and with regard to the drag-rise and buffet boundaries.
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Literature
Stanewsky, E. and Krogmann, P.: Transonic Drag Rise and Drag Reduction by Active / Passive Boundary Layer Control, AGARD Report No. 723, Special Course on Aircraft Drag Prediction and Reduction, July 1995.
Stanewsky, E., Délery, J., Fulker, J., Geissler, W. (Edit.): EUROSHOCK-Drag Reduction by Passive Shock Control, Notes on Numerical Fluid Mechanic, Volume 56, Verlag Vieweg & Sohn, 1997.
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© 1999 Springer Science+Business Media Dordrecht
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Stanewsky, E. (1999). Euroshock I and II: A Survey. In: Meier, G.E.A., Viswanath, P.R. (eds) IUTAM Symposium on Mechanics of Passive and Active Flow Control. Fluid Mechanics and its Applications, vol 53. Springer, Dordrecht. https://doi.org/10.1007/978-94-011-4199-4_6
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DOI: https://doi.org/10.1007/978-94-011-4199-4_6
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