Drag reduction on circular cylinders by ejecting jet from rear stagnation region
Subtitle: progress report for the period ending June 30, 1997 ... under Cooperative Agreement NCC1-232
By: by S. Atsuchi and S.N. Tiwari.
Contributors: Tiwari, S. N.; United States. National Aeronautics and Space Administration.
Series: NASA contractor report -- NASA CR-206329.
Publisher: Dept. of Mechanical Engineering, College of Engineering and Technology, Old Dominion University; National Aeronautics and Space Administration; National Technical Information Service, distributor
Published: 1997
Place of publication: Norfolk, Va; [Washington, DC; Springfield, Va
Language: eng
Format: Microform
Subjects: Drag reduction.; Circular cylinders.; Stagnation point.; Ejection.; Computational fluid dynamics.; Finite volume method.; Navier-Stokes equation.; Reynolds number.; Injection.; Pressure measurement.; Algorithms.
Notes: Shipping list no.: 98-0442-M.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1997] 2 microfiches. (NASA/CR ; 97-206329).