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- Effect of stabilizer location upon pitching and yawing moments in spins as shown by tests with the spinning balance
- Spinning characteristics of wings 1: rectangular Clark Y monoplane wing
- Aerodynamic Effects of a Split Flap on the Spinning Characteristics of a Monoplane Model
- The Aerodynamic Forces and Moments on a Spinning Model of the F4B-2 Airplane as Measured by the Spinning Balance
- Spinning Characteristics of Wings 2: Rectangular Clark Y Biplane Cellule: 25 Percent Stagger; 0 Degree Decalage; Gap/Chord 1.0
- Spinning characteristics of wings 4: changes in stagger of rectangular Clark Y cellules
- Spinning Characteristics of Wings 3: A Rectangular and Tapered Clark Y Monoplane Wing with Rounded Tips
- Spinning characteristics of the XN2Y-1 airplane obtained from the spinning balance and compared with results from the spinning tunnel and from flight tests
- Spinning characteristics of wings 5: N.A.C.A. 0009, 23018, and 6718 monoplane wings
- Wind-Tunnel Investigation of Effect of Yawing on Lateral-Stability Characteristics 2: Rectangular N.A.C.A. 23012 Wing with a Circular Fuselage and a Fin
- Wind-Tunnel Tests of Several Forms of Fixed Wing Slot in Combination With a Slotted Flap on an N.A.C.A. 23012 Airfoil
- Wind-tunnel investigation of effect of yaw on lateral-stability characteristics 1: four N.A.C.A. 23012 wings of various plan forms with and without dihedral