Design of the optimal nozzle of a hypersonic flight vehicle for given overall dimensions and moment

DOI10.1007/BF02698757zbMath0964.76077MaRDI QIDQ1567875

G. Yu. Misko

Publication date: 19 July 2000

Published in: Fluid Dynamics (Search for Journal in Brave)

zbMATH Keywords

isoperimetric conditionmoment constrainthypersonic ramjet enginelift optimizationmethod of indefinite control contouroptimal nozzlethrust optimization

Mathematics Subject Classification ID

Hypersonic flows (76K05) Flow control and optimization for compressible fluids and gas dynamics (76N25)

Related Items (1)

On the role of a balancing load in the problem of aerodynamic drag minimization in the supersonic flight regime

Cites Work

• Construction of asymmetric nozzles of maximum moment given additional conditions on the geometrical and force characteristics
• Optimization of a hypersonic ramjet power plant
• Variational problems of gas dynamics of nonequilibrium and equilibrium flows

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