APA (7th ed.) Citation

Anderson, B. T., & Meyer, R. R. (1990). Effects of wing sweep on in-flight boundary-layer transition for a laminar flow wing at Mach numbers from 0.60 to 0.79. National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility.

Chicago Style (17th ed.) Citation

Anderson, Bianca T., and Robert R. Meyer. Effects of Wing Sweep on In-flight Boundary-layer Transition for a Laminar Flow Wing at Mach Numbers from 0.60 to 0.79. Edwards, Calif.: National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility, 1990.

MLA (9th ed.) Citation

Anderson, Bianca T., and Robert R. Meyer. Effects of Wing Sweep on In-flight Boundary-layer Transition for a Laminar Flow Wing at Mach Numbers from 0.60 to 0.79. National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility, 1990.