Numerical study on influence of fuselage and stabilizer on control surface efficiency and interference characteristics for a hypersonic waverider-derived configuration

Engineering

• Numerical Study 100%
• Control Surface 100%
• Stabilizer 100%
• Key Parameter 10%
• Simulation Result 10%
• Reynolds-Averaged Navier-Stokes 10%
• Angle-of-Attack 10%
• Low Mach Number 10%
• Navier-Stokes Equation 10%
• Hypersonic Vehicle 10%
• Longitudinal Static Stability 10%
• Hypersonic Flows 10%
• Vehicle Design 10%
• Root Part 10%
• Surface Effectiveness 10%