Hypersonic Notes
- inviscid - laminar, low turbulence, low Reynolds number
Modern compressible flow : with historical perspective John David Anderson, Jr 1982 PSU QA911 .A6
Hypersonic and High Temperature Gas Dynamics
John David Anderson Jr 2000 AIAA page numbers in book, pdf+6 calorically perfect gas, γ = cp/cv = 1.4 ratio of specific heats p15 boundary layer thickness \delta ~ \propto ~ {M_∞}^2 / \sqrt{ R_{e_x} } where R_{e_x} is the local Reynolds number p19 convective heating q_c, radiative heating q_r 30% for Apollo p21 Knudsen number, Kn = \lambda/L where \lambda = mean free path, L = characteristic length Kn 0.001? to 0.3 Navier-Stokes p23 p surface pressure, \tau shear stress (viscous flow phenomena) p26 heat conduction q_w ~ = -k_w \left( { { \partial T } \over { \partial y } } \right)_w ... more in Part 2