Search Results for: Bodies Of Revolution With A Minimum Drag Factor And Low Heat Transfer At High Supersonic Flight Speeds

On the basis of the modified Newton theory and the theory of self-similar hypersonic flows, an investigation was made of the optimum shape of a body of revoluti

The optimal shape of a body of revolution with minimum drag at hypersonic velocities is investigated on the basis of modified Newtonian theory and theory of sel

An approximate method for determining the convective cooling requirement in the laminar-boundary-layer region of a body of revolution in high-speed flight was d