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Browsing by Author "Nonweiler, T."

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A method for numerical evaluation of the integral...

Nonweiler, T. (College of Aeronautics, Cranfield, )
A resume of maximum lift data for symmetrical wings, with various high-lift aids

Nonweiler, T. (College of Aeronautics, )
Incompressible flow past bodies of revolution

Nonweiler, T. (College of Aeronautics, )
Skin temperatures and heat transfer over wedge wings at extreme speeds of flight

Nonweiler, T. (College of Aeronautics, Cranfield, )
Surface conduction of the heat transferred from a boundary layer

Nonweiler, T. (College of Aeronautics, Cranfield, )
The air resistance of racing cyclists

Nonweiler, T. (College of Aeronautics, Cranfield, )
The laminar boundary layer in slip flow

Nonweiler, T. (College of Aeronuatics, Cranfield, )
The man-propelled aircraft: a preliminary assessment

Nonweiler, T. (College of Aeronautics, )
The numerical solution of certain differential equations occurring in Crocco's theory of the laminar boundary layer

Kirkby, S.; Nonweiler, T. (College of Aeronautics, Cranfield, )
The theoretical wave drag at zero lift of fully-tapered swept wings of arbitrary section

Nonweiler, T. (College of Aeronautics, Cranfield, )
The two-dimensional laminar boundary layer at hypersonic speeds

Nonweiler, T. (College of Aeronautics, Cranfield, )
The wave drag of highly-swept wings: a comparison of linear theory and slender body theory

Nonweiler, T. (College of Aeronautics, )
Theoretical stability derivatives of a highly swept delta wing and slender body combination

Nonweiler, T. (College of Aeronautics, Cranfield, )

Browsing by Author "Nonweiler, T."

Browsing by Author "Nonweiler, T."

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