TY - BOOK ID - 145395076 TI - Effect of shortening transition liner to decrease overall length of a ram induction combustor AU - Schultz, Donald F. AU - Perkins, Porter J. AU - Wear, Jerrold D. AU - United States. AU - Lewis Research Center. PY - 1970 PB - Washington, D.C. : National Aeronautics and Space Administration, DB - UniCat KW - Turbojet engines. KW - Combustion chambers. KW - Airplanes KW - Smoke. KW - Combustion KW - Airplanes KW - Combustion chambers KW - Combustion KW - Smoke. KW - Turbojet engines KW - Combustion. KW - Research. KW - Turbojet engines KW - Combustion. KW - Testing. KW - Research. UR - https://www.unicat.be/uniCat?func=search&query=sysid:145395076 AB - ER -