Books by Douglas E. Harrington:
Books in the extended shelves:
![[X-Info]](https://onlinebooks.library.upenn.edu/infouc.gif)
Harrington, Douglas E.: Cold-flow performance of several variations of a ram-air-cooled plug nozzle for supersonic-cruise aircraft (National Aeronautics and Space Administration ;, 1974), also by David M. Straight, Stanley M. Nosek, and Lewis Research Center (page images at HathiTrust)- Harrington, Douglas E.: 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 Research Center's proposed altitude wind tunnel (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1987), also by Richard R. Burley and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
- Harrington, Douglas E.: Experimental evaluation of honeycomb/screen configurations and short contraction section for NASA Lewis Research Center's altitude wind tunnel (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1987), also by Richard R. Burley and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
- Harrington, Douglas E.: Experimental evaluation of wall Mach number distributions of the octagonal test section proposed for NASA Lewis Research Center's altitude wind tunnel (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1986), also by Robert R. Corban, Richard R. Burley, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
- Harrington, Douglas E.: Thrust performance of isolated 36-chute suppressor plug nozzles with and without ejectors at Mach numbers from 0 to 0.45 (National Aeronautics and Space Administration ;, 1975), also by Stanley A. Skebe, James J. Schloemer, and Lewis Research Center (page images at HathiTrust)
- Harrington, Douglas E.: Thrust performance of isolated two dimension suppressed plug nozzles with and without ejectors at mach numbers from 0 to 0.45 (U.S. National Aeronautics and Space Administration ;, 1976), also by Stanley A. Skebe, James J. Schloemer, United States National Aeronautics and Space Administration, and Lewis Research Center (page images at HathiTrust)
Find more by Douglas E. Harrington at your library, or elsewhere.