Axisymmetric nose shapes of specified aspect ratio, optimum or close to optimum with respect to wave drag

DOI10.1016/S0021-8928(03)90043-8zbMath1151.70334OpenAlexW2070905559MaRDI QIDQ5318141

N. I. Tillyaeva, A. N. Krajko, K. S. P'yankov, D. E. Pudovikov

Publication date: 21 September 2005

Published in: Journal of Applied Mathematics and Mechanics (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1016/s0021-8928(03)90043-8

zbMATH Keywords

axisymmetric nose conesoptimal drag

Mathematics Subject Classification ID

Variable mass, rockets (70P05) Hypersonic flows (76K05)

Related Items (7)

Pointed two-parameter power-law nose shapes of minimum wave drag ⋮ Optimal axisymmetric noses of bodies in a flow. Calculations and experiments ⋮ A criterion for minimum wave drag of a body ⋮ Newton's problem of the optimal forebody: history of the solution ⋮ Analytical solution to the wave-drag minimization problem for an axisymmetric fore-body using local linearization ⋮ Truncated power-law bodies as a result of an approximate solution to the Newton problem on a body having the minimum drag ⋮ Nose part of the body of revolution having minimum aerodynamic drag in the range of large subsonic velocities

Cites Work

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• Homogeneous form of the Navier-Stokes equation for plane-parallel steady flows of an incompressible fluid
• Construction of airfoils and engine nacelles that are supercritical in a transonic perfect-gas flow
• On a class of bodies of revolution witb minimum wave resistance
• Determination of the shape of a body of minimum drag at hypersonic speed
• Methods of increasing the accuracy in Godunov's scheme
• Monotonic scheme of the second order of approximation for the continuous calculation of non-equilibrium flows
• Pointed two-parameter power-law nose shapes of minimum wave drag
• On the solution of variational problems of supersonic gas dynamics
• Variational problems for supersonic bodies of revolution and nozzles

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