Books by Robert L. Stallings:
Books in the extended shelves:
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Stallings, Robert L.: Aerodynamic characteristics of a Sparrow III missile model in the flow field of a generalized parent body at Mach 2.86 (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1984), also by United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)- Stallings, Robert L.: Analysis of the performance of the drive system and diffuser of the Langley Unitary Plan Wind Tunnel (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), also by Lowell E. Hasel, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and Langley Research Center (page images at HathiTrust)
- Stallings, Robert L.: Effect of passive venting on static pressure distributions in cavities at subsonic and transonic speeds (National Aeronautics and Space Administration, Langley Research Center, 1994), also by United States National Aeronautics and Space Administration (page images at HathiTrust)
- Stallings, Robert L.: Effect of Reynolds number on stability characteristics of a cruciform wing-body at supersonic speeds (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1980), also by Carolyn B. Watson, Milton Lamb, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
- Stallings, Robert L.: Effects of roughness size on the position of boundary-layer transition and on the aerodynamics characteristics of a 55 ̊swept delta wing at supersonic speeds (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1977), also by Milton Lamb and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
- Stallings, Robert L.: Experimental cavity pressure distributions at supersonic speeds (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1987), also by Floyd J. Wilcox and Langley Research Center (page images at HathiTrust)
- Stallings, Robert L.: Experimental heat-transfer distributions on a blunt lifting body at Mach 3.71 (National Aeronautics and Space Administration ;, 1970), also by Ida K. Collins, Robert L. Wright, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
- Stallings, Robert L.: Heat-transfer distributions on a 0.013-scale shuttle solid rocket booster at Mach 3.70 and angles of attack from 0 ̊to 180 ̊ (National Aeronautics and Space Administration ;, 1976), also by Milton Lamb, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
- Stallings, Robert L.: Helium concentrations downstream of a vent exhausting helium at sonic velocity into a supersonic stream of air at Mach numbers of 3.51 and 4.50 (National Aeronautics and Space Administration, 1963), also by Paul W. Howard, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
- Stallings, Robert L.: Measurements of forces, moments, and pressures on a generic store separating from a box cavity at supersonic speeds (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ;, 1991), also by Dana K. Forrest, Floyd J. Wilcox, and Langley Research Center (page images at HathiTrust)
- Stallings, Robert L.: NASA TN D-5392 (National Aeronautics and Space Administration ;, 1969), also by Dorothy T. Howell, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
- Stallings, Robert L.: Sweep effect on the drag of rows of perpendicular circular cylinders in a laminar boundary layer at supersonic free-stream velocities (National Aeronautics and Space Administration ;, 1974), also by Milton Lamb and Langley Research Center (page images at HathiTrust)
- Stallings, Robert L.: Wind-tunnel measurements and comparison with flight of the boundary layer and heat transfer on a hollow cylinder at Mach 3 (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1980), also by Milton Lamb, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
- Stallings, Robert L.: Wing-alone aerodynamic characteristics for high angles of attack at supersonic speeds (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), also by Milton Lamb, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
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