TY - BOOK ID - 138095885 TI - Effect of unit Reynolds number, nose bluntness, angle of attack, and roughness on transition on a 5° half-angle cone at Mach 8 AU - Stainback, P. Calvin AU - United States. PY - 1969 PB - Washington, D.C. : National Aeronautics and Space Administration, DB - UniCat KW - Aerodynamics, Hypersonic. UR - https://www.unicat.be/uniCat?func=search&query=sysid:138095885 AB - ER -