Author: William R. Wells Publisher: ISBN: Category : Aerodynamics Languages : en Pages : 312
Book Description
Newtonian closed-form expressions for the aerodynamic coefficients are developed for complete and partial conic and spheric bodies at combined angles of attack and sideslip. Calculations from these expressions are presented in tabulated form for various body shapes. Closed-form expressions for some of the static stability derivatives are also presented. Comparisons of this theory with hypersonic experimental data are made for many of the body shapes.
Author: United States. National Aeronautics and Space Administration. Scientific and Technical Information Division Publisher: ISBN: Category : Aeronautics Languages : en Pages : 258
Author: United States. National Aeronautics and Space Administration Scientific and Technical Information Division Publisher: ISBN: Category : Aeronautics Languages : en Pages : 262
Author: M.K. Singh Publisher: Springer ISBN: 9811053294 Category : Technology & Engineering Languages : en Pages : 691
Book Description
The book presents high-quality papers presented at 3rd International Conference on Applications of Fluid Dynamics (ICAFD 2016) organized by Department of Applied Mathematics, ISM Dhanbad, Jharkhand, India in association with Fluid Mechanics Group, University of Botswana, Botswana. The main theme of the Conference is "Sustainable Development in Africa and Asia in context of Fluid Dynamics and Modeling Approaches". The book is divided into seven sections covering all applications of fluid dynamics and their allied areas such as fluid dynamics, nanofluid, heat and mass transfer, numerical simulations and investigations of fluid dynamics, magnetohydrodynamics flow, solute transport modeling and water jet, and miscellaneous. The book is a good reference material for scientists and professionals working in the field of fluid dynamics.
Author: Robert H. Feldhuhn Publisher: ISBN: Category : Angle of attack (Aerodynamics) Languages : en Pages : 148
Book Description
Pressure, heat transfer, force, flow field surveys and flow visualization measurements on an inclined cone were obtained in a wind tunnel at a nominal Mach number of 6. Force measurements were also obtained for a 2/3 power law body and two ducted-cone configurations.
Author: William R. Wells
Author: William R. Wells
Author: William R. Wells
Author: United States. National Aeronautics and Space Administration. Scientific and Technical Information Division
Author: United States. National Aeronautics and Space Administration Scientific and Technical Information Division
Author: 
Author: 
Author: Charles L. Ladson
Author: M.K. Singh
Author: Robert H. Feldhuhn