Computation of Supersonic Flow over Flying Configurations

5

The Aerodynamical Characteristics of Flying Configurations with Arbitrary Shapes, in Supersonic Flow

Contents

5.1 General considerations

5.2 The computation of the aerodynamical characteristics of the delta wings

5.3 The computation of the aerodynamical characteristics of delta wing-fuselage configurations

5.4 The computation of the aerodynamical characteristics of delta wing-fuselage configurations, fitted with leading edge flaps, in open positions

5.5 The computation of the lift, pitching moment and drag coefficients of the rectangular wings

5.6 Conclusions

5.1. General considerations

In this chapter the aerodynamic characteristics, i.e. the lift coefficient C, the pitching moment coefficient C_m and the drag coefficient C_d⁽ⁱ⁾ of the ...