High-Fidelity Aerothermal Engineering Analysis for Planetary Probes Using DOTNET Framework and OLAP Cubes Database

Figure 15

(a)–(f) Trajectory data: flight velocity, stagnation point heating, deceleration versus altitude.

(a) Flight velocity with altitude

(b) Reynolds number versus altitude

(c) Stagnation point pressure versus altitude

(d) Deceleration versus altitude

(e) Stagnation point heat versus altitude

(f) Stagnation point heat versus time