Performance of a vortex-controlled diffuser in an annular swirl-can combustor at inlet Mach numbers up to 0.53
Title:
Performance of a vortex-controlled diffuser in an annular swirl-can combustor at inlet Mach numbers up to 0.53
Author:
Smith, John M. (John Milton), 1922-
Personal Author:
Publication Information:
[Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Office, 1979.
Physical Description:
14 pages : illustrations ; 28 cm.
Language:
English
Format :
Book