Wind tunnel tests of wings at Reynolds numbers below 70 000 von LAITONE, E. V

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Fixed-Pitch Propeller Selection for Light Airplanes von Laitone, E. V

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Aerodynamic lift at Reynolds numbers below 7 x 10 exp 4 von Laitone, E. V

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Comment on "Analytic V Speeds from Linearized Propeller Polar" von Laitone, E. V

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Tail load calculations for light airplanes von Laitone, E. V

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Comment on 'Drag reduction factor due to ground effect' von Laitone, E. V

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Lift-curve slope for finite-aspect-ratio wings von Laitone, E. V

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Rate of climb for light propeller powered airplanes von Laitone, E. V

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Prandtl's biplane theory applied to canard and tandem aircraft von Laitone, E. V

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Performance estimation for light propeller airplanes von Laitone, E. V

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Performance prediction for light airplanes von Laitone, E. V

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Ideal Tail Load for Minimum Aircraft Drag von Laitone, E. V

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Positive Tail Loads for Minimum Induced Drag of Subsonic Aircraft von Laitone, E.V

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Errors in the numerical integration of a linearized equation for particle flows von Laitone, J.A, Laitone, E.V

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The second approximation to cnoidal and solitary waves von Laitone, E. V.

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Effect of Thrust on the Longitudinal Oscillations of Missiles von LAITONE, E. V, LIN, WEN-FAN

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Aerodynamic lift at Reynolds numbers below 7 times 10(4) von Laitone, E V

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THE SUBSONIC FLOW ABOUT A BODY OF REVOLUTION von LAITONE, E. V.

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Reply by Author to R. S. Shevell von Laitone, E. V

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Phugoid oscillations at hypersonic speeds von CHOU, Y. S, LAITONE, E. V

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