Oscillatory-derivative measurements on sting-mounted wind-tunnel models : method of test and results for pitch and yaw on a cambered ogee wing at mach numbers up to 2.6.
Thompson, J. S.,author.
Fail, R. A.,author.
Great Britain.Her Majesty's Stationery Office.
Aeronautical Research Council (Great Britain),issuing body.
July 1962.