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title: National Advisory Committee for Aeronautics -- Reports
On the theory of wing sections with particular reference to the lift distribution
Interference on airfoil of finite span in open rectangular wing tunnel
General potential theory of arbitrary wing sections
Vibration response of airplane structures
Improved airplane windshields to provide vision in stormy weather
Characteristics of N.A.C.A. 23012 airfoil from tests in full-scale and variable-density tunnels
Propeller vibrations and effect of centrifugal force
Full-scale tests of new type N.A.C.A. nose-slot cowling
Full-scale tests of new type N.A.C.A. nose-slot cowling
Full-scale tests of new type N.A.C.A. nose-slot cowling
Full-scale tests of N.A.C.A. Cowlings
Full-scale tests of N.A.C.A. cowlings
Full-scale tests of N.A.C.A. cowlings
Characteristics of six propellers including high-speed range
Characteristics of six propellers including high speed range
Characteristics of six propellers including high-speed range
Cooling of airplane engines at low air speeds
Cooling of airplane engines at low air speeds
Nonstationary flow about Wing-Aileron-Tab combination including aerodynamic balance
Airfoil-contour modifications based on Epsilon-curve method of calculating pressure distribution
Effect of lift coefficient on propeller flutter
Problem of noise reduction with reference to light airplanes