APA (7th ed.) Citation

Hall, I. M., & Rogers, E. W. E. (1962). Part I: The flow pattern on a tapered swept-back wing at Mach numbers between 0.6 and 1.6. Part II: Experiments with a tapered swept-back wing of Warren 12 planform at Mach numbers between 0.6 and 1.6. Her Majesty's Stationery Office.

Chicago Style (17th ed.) Citation

Hall, Ian Murray, and E. W. E. Rogers. Part I: The Flow Pattern on a Tapered Swept-back Wing at Mach Numbers Between 0.6 and 1.6. Part II: Experiments with a Tapered Swept-back Wing of Warren 12 Planform at Mach Numbers Between 0.6 and 1.6. London: Her Majesty's Stationery Office, 1962.

MLA (9th ed.) Citation

Hall, Ian Murray, and E. W. E. Rogers. Part I: The Flow Pattern on a Tapered Swept-back Wing at Mach Numbers Between 0.6 and 1.6. Part II: Experiments with a Tapered Swept-back Wing of Warren 12 Planform at Mach Numbers Between 0.6 and 1.6. Her Majesty's Stationery Office, 1962.