TY - CONF T1 - Prediction of Transition Location and Its Effects on Shock Bump Control on a Natural Laminar Flow Aerofoil PY - 2011/06/05 AU - Deng F AU - McIntosh SC AU - Qin N ED - DO - DOI: 10.1007/978-3-642-25685-1_39 PB - Springer Berlin Heidelberg SN - 9783642256844 SP - 251 EP - 256 Y2 - 2025/04/09 ER -