Print Email Facebook Twitter On the application of boundary layer control to a slender wing supersonic airliner cruising at M = 2.2 Title On the application of boundary layer control to a slender wing supersonic airliner cruising at M = 2.2 Author Craven, A.H. Hopkins, H.L. Institution College of Aeronautics Cranfield Date 1962-04-01 Abstract The College of Aeronautics was founded in 1946 and was granted university status in 1969 becoming the Cranfield Institute of Technology. In 1993 it changed its name to Cranfield University. To reference this document use: http://resolver.tudelft.nl/uuid:26955549-9a30-40b9-8a70-5dd02e5ba05c Publisher College of Aeronautics Cranfield Source College of Aeronautics Report 157 Part of collection Aerospace Engineering Reports Document type report Rights (c) 1962 College of Aeronautics Cranfield Files PDF CoA_Report_No.157.pdf 10.36 MB Close viewer /islandora/object/uuid:26955549-9a30-40b9-8a70-5dd02e5ba05c/datastream/OBJ/view