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Last edited by ImportBot
August 31, 2008 | History

Harry W. Carlson

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  • Cover of: Estimation of leading-edge thrust for supersonic wings of arbitrary planform

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  • Cover of: Simplifed sonic-boom prediction

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  • Cover of: wind-tunnel study of the applicability of far-field sonic-boom theory to the space shuttle orbiter

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  • Cover of: Applicability of linearized-theory attached-flow methods to design and analysis of flap systems at low speeds for thin swept wings with sharp leading edges

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  • Cover of: Estimation of attainable leading-edge thrust for wings at subsonic and supersonic speeds

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  • Cover of: study of the sonic-boom characteristics of a blunt body at a Mach number of 4.14

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  • Cover of: Survey and analysis of research on supersonic drag-due-to-lift minimumization with recommendations for wing design

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  • Cover of: Validation of a computer code for analysis of subsonic aerodynamic performance of wings with flaps in combination with a canard or horizontal tail and an application of optimization

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  • Cover of: Application of an aerodynamic analysis method including attainable thrust estimates to low speed leading-edge flap design for supersonic cruise vehicles

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  • Cover of: The design and analysis of simple low speed flap systems with the aid of linearized theory computer programs

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  • Cover of: Improved method for prediction of attainable wing leading-edge thrust

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  • Cover of: modification to linearized theory for prediction of pressure loadings on lifting surfaces at high supersonic Mach numbers and large angles of attack

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  • Cover of: Simplified sonic-boom prediction.

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  • Cover of: Survey and analysis of research on supersonic drag-due-to-lift minimization with recommendations for wing design

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  • Cover of: Validation of a computer code for analysis of subsonic aerodynamic performance of wings with flaps in combination with a canard or horizontal tail and an application to optimization

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  • Cover of: Validation of a pair of computer codes for estimation and optimization of subsonic aerodynamic performance of simple hinged-flap systems for thin swept wings

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August 31, 2008 Created by ImportBot Imported from Talis record