The Online Books Page

Books by Delma C. Freeman:

Books in the extended shelves:

• Freeman, Delma C.: Comparison of space shuttle orbiter low-speed static stability and control derivatives obtained from wind-tunnel and approach and landing flight tests (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1980), also by Bernard Spencer, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Freeman, Delma C.: Dynamic stability characteristics of the combination space shuttle orbiter and ferry vehicle (National Aeronautics and Space Administration ;, 1977), also by Richmond P. Boyden and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Freeman, Delma C.: Dynamic stability derivatives of space shuttle orbiter from wind-tunnel and approach and landing flight tests (National Aeronautics and Space Administration , Scientific and Technical Information Office ;, 1980), also by Langley Research Center and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Freeman, Delma C.: Effects of relaxed static longitudinal stability on a single-stage-to-orbit vehicle design (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1979), also by Alan W. Wilhite and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Freeman, Delma C.: Low subsonic flight and force investigation of a supersonic transport model with a double-delta wing (National Aeronautics and Space Administration, 1968), also by Langley Research Center and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Freeman, Delma C.: Low subsonic flight and force investigation of a supersonic transport model with a highly swept arrow wing (National Aeronautics and Space Administration, 1967), also by Langley Research Center (page images at HathiTrust)
• Freeman, Delma C.: NASA TN D-5408 (National Aeronautics and Space Administration ;, 1969), also by Richard D'Amato, Sue B. Grafton, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Freeman, Delma C.: Static aerodynamic characeristics of a winged single-stage-to-orbit vehicle at Mach numbers from 0.3 to 4.63 (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), also by Roger H. Fournier, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Freeman, Delma C.: Static aerodynamic characteristics of a single-stage-to-orbit vehicle with low planform loading at Mach numbers from 0.3 to 4.63 (Scientific and Techn. Information Off., NASA, 1977), also by Roger H. Fournier (page images at HathiTrust)
• Freeman, Delma C.: Subsonic and transonic dynamic stability characteristics of a space shuttle orbiter (National Aeronautics and Space Administration ;, 1975), also by Richmond P. Boyden and Langley Research Center (page images at HathiTrust)
• Freeman, Delma C.: Subsonic and transonic dynamic-stability characteristics of the space shuttle launch vehicle (U.S. National Aeronautics and Space Administration ;, 1976), also by Edwin E. Davenport, Richmond P. Boyden, and Langley Research Center (page images at HathiTrust)
• Freeman, Delma C.: Supersonic dynamic stability characteristics of a space shuttle orbiter (National Aeronautics and Space Administration ;, 1976), also by Edwin E. Davenport, Richmond P. Boyden, and Langley Research Center (page images at HathiTrust)
• Freeman, Delma C.: Supersonic dynamic-stability derivatives of the space shuttle launch vehicle (National Aeronautics and Space Administration ;, 1976), also by Richmond P. Boyden, Edwin E. Davenport, and Langley Research Center (page images at HathiTrust)
• Freeman, Delma C.: Wind-tunnel investigation of a jet transport airplane configuration with an external-flow jet flap and inboard pod-mounted engines (National Aeronautics and Space Administration, 1970), also by Lysle P. Parlett and Robert L. Henderson (page images at HathiTrust)
• Freeman, Delma C.: Wind-tunnel investigation of a jet transport airplane configuration with high thrust-weight ratio and an external-flow jet flap (National Aeronautics and Space Administration; [for sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Va.], 1970), also by Lysle P. Parlett and Charles Christian Smith (page images at HathiTrust)

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