Experimental evaluation of wall Mach number distributions of the octagonal test section proposed for NASA Lewis Research Center's altitude wind tunnel /

by Harrington, Douglas E.
Published 1986

Thrust performance of isolated two dimension suppressed plug nozzles with and without ejectors at mach numbers from 0 to 0.45 /

by Harrington, Douglas E., Schloemer, James J., Skebe, Stanley A.
Published 1976

Experimental evaluation of blockage ratio and plenum evacuation system flow effects on pressure distribution for bodies of revolution in 0.1-scale model test section of NASA Lewis...

by Burley, Richard R.
Published 1987

Experimental evaluation of honeycomb/screen configurations and short contraction section for NASA Lewis Research Center's altitude wind tunnel /

by Burley, Richard R.
Published 1987