TY - BOOK ID - 137107254 TI - Feasibility and benefits of laminar flow control on supersonic cruise airplanes AU - Powell, A. G. AU - Agrawal, Sudhir. AU - Lacey, T. R. AU - Langley Research Center. PY - 1989 PB - Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, DB - UniCat UR - https://www.unicat.be/uniCat?func=search&query=sysid:137107254 AB - ER -