Transonic wind-tunnel investigation of the effects of sweepback and thickness ratio on the wing loads of a wing-body combination of aspect ratio 4 and taper ratio 0.6

Author: Platt, Robert J.
Additional Authors: Brooks, Joseph D.
Year: 1955
Document Type: MAIN
SUDOC: Y 3.N 21/5:15/L54L31b
Series: NACA research memorandum ;
Report Number: L54L31b
Subjects: Charts, diagrams, etc
Aerodynamic load
Wind tunnel testing
Airplanes--Fuselage
Airplanes--Wings, Swept-back
Aerodynamics, Transonic
Link: https://hdl.handle.net/2027/mdp.39015095100858

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