The Online Books Page

Books by Hugh A. Klassen:

Books in the extended shelves:

• Klassen, Hugh A.: Effect of inducer inlet and diffuser throat areas on performance of a low pressure ratio sweptback centrifugal compressor (National Aeronautics and Space Administration ;, 1975), also by Lewis Research Center (page images at HathiTrust)
• Klassen, Hugh A.: Experimental performance of a 13.65-centimeter-tip-diameter tandem-bladed sweptback centifugal compressor designed for a pressure ratio of 6 (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1977), also by Lawrence F. Schumann, Jerry R. Wood, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Klassen, Hugh A.: Experimental performance of a 16.10-centimeter-tip-diameter sweptback centrifugal compressor designed for a 6:1 pressure ratio (National Aeronautics and Space Administration ;, 1977), also by Lawrence F. Schumann, Jerry R. Wood, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Klassen, Hugh A.: Performance in air of 4-inch- (10.16-cm- ) mean-diameter single-stage axial-flow turbine for Reynolds numbers from 4900 to 188,000 (National Aeronautics and Space Administration ;, 1968), also by Robert Y. Wong and Lewis Research Center (page images at HathiTrust)
• Klassen, Hugh A.: Performance of a low-pressure-ratio centrifugal compressor with four diffuser designs (National Aeronautics and Space Administration ;, 1973), also by Lewis Research Center (page images at HathiTrust)

Find more by Hugh A. Klassen at your library, or elsewhere.