SYSTEMATIC WIND TUNNEL TESTS WITH SLATS ON A 10 PER CENT THICK SYMMETRICAL WING SECTION (EQ 1040 PROFILE)

Subjects

Airplanes - Design and Construction|Wings

Links

http://naca.central.cranfield.ac.uk/reports/arc/rm/2705.pdf

Record Type

ONLINE

Corporate Author

Aeronautical Research Council London

Author

Moss, G F

Publication Date

2022

Collection