Dobson, M. D. (1970). Tests at a mach number of 2.0 on a rectangular twin-duct air intake with variable geometry: Situated in the flow field of a slender wing. H.M. Stationery Off.
Chicago Style (17th ed.) CitationDobson, M. D. Tests at a Mach Number of 2.0 on a Rectangular Twin-duct Air Intake with Variable Geometry: Situated in the Flow Field of a Slender Wing. London: H.M. Stationery Off, 1970.
MLA (9th ed.) CitationDobson, M. D. Tests at a Mach Number of 2.0 on a Rectangular Twin-duct Air Intake with Variable Geometry: Situated in the Flow Field of a Slender Wing. H.M. Stationery Off, 1970.
Warning: These citations may not always be 100% accurate.