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Theorie
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A simple method of estimating the subsonic lift and damping in roll of sweptback wings
On compressibility corrections for subsonic flow over bodies of revolution
Ambient pressure determination at high altitudes by use of free-molecule theory
The influence of blade-width distribution on propeller characteristics
Free-space oscillating pressures near the tips of rotating propellers
Theoretical investigation of transonic similarity for bodies of revolution
Estimation of the damping in roll of supersonic-leading-edge wing-body combinations
The Calculation of Downwash Behind Wings of Arbitrary Plan Form at Supersonic Speeds
Calculation of compressible potential flow past slender bodies of revolution by an integral method
The interpretation of biaxial-tension experiments involving constant stress ratios
A method of computing subsonic flows around given airfoils
Calculation of transonic flows past thin airfoils by integral method
First-order theory for unsteady motion of thin wings at supersonic speeds
Supersonic flow around circular cones at angles of attack
Three-dimensional, unsteady-lift problems in high-speed flight : basic concepts
A Survey of the Flow at the Plane of the Propeller of a Twin-engine Airplane
On the continuation of a potential gas flow across the sonic line
Theory of Helicopter Damping in Pitch or Roll and a Comparison With Flight Measurements
Correspondence flows for wings in linearized potential fields at subsonic and supersonic speeds
Similarity laws for transonic flow about wings of finite span
On the use of coupled modal functions in flutter analysis
Resistance of a delta wing in a supersonic flow
Applications of Von Karman's integral method in supersonic wing theory
Charts and Tables for Use in Calculations of Downwash of Wings of Arbitrary Plan Form
Damping in roll of cruciform and some related delta wings at supersonic speeds
Rolling and yawing moments for swept-back wings in sideslip at supersonic speeds
A plan-form parameter for correlating certain aerodynamic characteristics of swept wings
Axial-momentum theory for propellers in compressible flow