TY - BOOK ID - 135987407 TI - Experimental study of nozzle wall boundary layers at Mach numbers 20 to 47 AU - Kemp, Joseph H. AU - Owen, F. Kevin AU - United States. PY - 1972 PB - Washington, D.C. : National Aeronautics and Space Administration, DB - UniCat KW - Wall pressure (Aerodynamics) KW - Aerodynamics, Hypersonic. UR - https://www.unicat.be/uniCat?func=search&query=sysid:135987407 AB - ER -