An Evaluation of Linearized Vortex Theory as Applied to Single and Multiple Rotors Hovering in and Out of Ground Effect

An Evaluation of Linearized Vortex Theory as Applied to Single and Multiple Rotors Hovering in and Out of Ground Effect
Title An Evaluation of Linearized Vortex Theory as Applied to Single and Multiple Rotors Hovering in and Out of Ground Effect PDF eBook
Author Harry H. Heyson
Publisher
Pages 70
Release 1959
Genre Linear systems
ISBN

Download An Evaluation of Linearized Vortex Theory as Applied to Single and Multiple Rotors Hovering in and Out of Ground Effect Book in PDF, Epub and Kindle

An Evaluation of Linearized Vortex Theory as Applied to Single and Multiple Rotors Hovering in and Out of Ground Effect

An Evaluation of Linearized Vortex Theory as Applied to Single and Multiple Rotors Hovering in and Out of Ground Effect
Title An Evaluation of Linearized Vortex Theory as Applied to Single and Multiple Rotors Hovering in and Out of Ground Effect PDF eBook
Author Harry H. Heyson
Publisher
Pages 66
Release 1959
Genre Linear systems
ISBN

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Index of NASA Technical Publications

Index of NASA Technical Publications
Title Index of NASA Technical Publications PDF eBook
Author
Publisher
Pages 494
Release 1959
Genre Aeronautics
ISBN

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Index of NASA Technical Publications

Index of NASA Technical Publications
Title Index of NASA Technical Publications PDF eBook
Author United States. National Aeronautics and Space Administration
Publisher
Pages 500
Release 1959
Genre Aeronautics
ISBN

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Index of NACA Technical Publications

Index of NACA Technical Publications
Title Index of NACA Technical Publications PDF eBook
Author United States. National Advisory Committee for Aeronautics
Publisher
Pages 860
Release 1957
Genre Aeronautics
ISBN

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NASA Technical Note

NASA Technical Note
Title NASA Technical Note PDF eBook
Author
Publisher
Pages 1070
Release 1974
Genre
ISBN

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Fixed and Flapping Wing Aerodynamics for Micro Air Vehicle Applications

Fixed and Flapping Wing Aerodynamics for Micro Air Vehicle Applications
Title Fixed and Flapping Wing Aerodynamics for Micro Air Vehicle Applications PDF eBook
Author Thomas J. Mueller
Publisher AIAA
Pages 614
Release 2001
Genre Aerodynamics
ISBN 9781600864469

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This title reports on the latest research in the area of aerodynamic efficency of various fixed-wing, flapping wing, and rotary wing concepts. It presents the progress made by over fifty active researchers in the field.