Aerodynamic characteristics of \(V\)-shaped wings with shock waves detached from leading edges at hypersonic speeds

DOI10.1007/BF01342691zbMath0788.76053OpenAlexW1964096878MaRDI QIDQ1316803

N. A. Ostapenko

Publication date: 12 April 1994

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

Full work available at URL: https://doi.org/10.1007/bf01342691

zbMATH Keywords

direct problemlift-drag ratioreduced normal force coefficient

Mathematics Subject Classification ID

Shock waves and blast waves in fluid mechanics (76L05) Hypersonic flows (76K05)

Related Items (3)

Hypersonic flow past conical V-shaped wings ⋮ Lifting wings of optimum shape in a viscous hypersonic stream ⋮ Lift-drag ratio of a hypersonic waverider of delta planform

Cites Work

• Unnamed Item
• Optimization of the spatial shape of load-carrying bodies of small elongation at hypersonic velocities
• Hypersonic flow past delta wing of finite thickness
• Hypersonic flow past a delta wing
• Unsteady hypersonic flow over delta wings with detached shock waves
• Hypersonic flow with attached shock waves over plane delta wings
• Thickness effect on the force of slender delta wings in hypersonic flow
• A wing with the maximum lift/drag ratio at supersonic velocity
• LIFT OF SLENDER DELTA WINGS ACCORDING TO NEWTONIAN THEORY

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