Program for the design of an axial compressor stage based on the radial equilibrium equations
Papailiou, Kyriacos D.
MetadataShow full item record
A computer program is presented to determine the three-dimensional flow conditions in an axial flow compressor stage. Entropy and energy gradients are taken into account as well as the radial shift and the curvatures of the axisymmetric stream surfaces. The program can be used at elevated Mach numbers since shock losses and compressibility effects are included. It represents an extension of work done for a research program to investigate the tip clearance effects in a three-stage compressor
NPS Report NumberNPS57PY71091A
Showing items related by title, author, creator and subject.
Agrawal, B.N. (2005);This paper presents a review of the spacecraft design program at the Naval Postgraduate School. This program is part of the space systems engineering curriculum. In this curriculum, the students take at least one course ...
Klee, Charles W., Jr. (Boston, Massachusetts; Boston University, 1968-06);Over the past several years the United States Atlantic Fleet Anphib1ous Force has been faced with increasing losses of qualified enlisted men. In 1965 the Atlantic Fleet Amphibious Force had more men leaving the Navy than ...
Shick, BethAnn. (Monterey, California. Naval Postgraduate School, 2007-12);The Joint Strike Fighter (JSF) program is the largest Department of Defense (DoD) military aircraft acquisition program to date. The JSF will serve the Air Force, Navy and Marine Corps, as well as many of our key ...