Thompson, J. S. (1964). 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. Her Majesty's Stationery Office.
Chicago Style (17th ed.) CitationThompson, J. S. 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. London: Her Majesty's Stationery Office, 1964.
MLA (9th ed.) CitationThompson, J. S. 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. Her Majesty's Stationery Office, 1964.
Warning: These citations may not always be 100% accurate.