Books by Ronald G. Huff:
Books in the extended shelves:
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Huff, Ronald G.: Characteristics of five ejector configurations at free-stream mach numbers from 0 to 2.0 (National Aeronautics and Space Administration, 1959), also by John L. Klann and United States National Aeronautics and Space Administration (page images at HathiTrust)- Huff, Ronald G.: Cold-flow acoustic evaluation of a small-scale, divergent, lobed nozzle for supersonic jet noise suppression (National Aeronautics and Space Administration ;, 1975), also by Donald E. Groesbeck and Lewis Research Center (page images at HathiTrust)
- Huff, Ronald G.: Comparison of jet Mach number decay data with a correlation and jet spreading contours for a large variety of nozzles (National Aeronautics and Space Administration ;, 1977), also by Donald E. Groesbeck, Uwe H. von Glahn, and United States National Aeronautics and Space Administration (page images at HathiTrust)
- Huff, Ronald G.: Convective heat-transfer coefficients from a solution of the conduction equation for a wall separating two fluids, one having an oscillating temperature (National Aeronautics and Space Administration ;, 1969), also by United States National Aeronautics and Space Administration and Lewis Research Center (page images at HathiTrust)
- Huff, Ronald G.: NASA TN D-5168 (National Aeronautics and Space Administration ; [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1969), also by Lewis Research Center and United States National Aeronautics and Space Administration (page images at HathiTrust)
- Huff, Ronald G.: NASA TN D-5291 (National Aeronautics and Space Administration ; [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1969), also by Lewis Research Center and United States National Aeronautics and Space Administration (page images at HathiTrust)
- Huff, Ronald G.: NASA TN D-6422 (National Aeronautics and Space Administration ;, 1971), also by Frank B. Molls, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
- Huff, Ronald G.: Performance of external-compression bump inlet at Mach numbers of 1.5 to 2.0 (National Advisory Committee for Aeronautics, 1957), also by Paul C. Simon, Dennis W. Brown, Lewis Flight Propulsion Laboratory, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
- Huff, Ronald G.: Simplified combustion noise theory yielding a prediction of fluctuating pressure level (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1984), also by United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
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