The Online Books Page

Low Speed

See also what's at your library, or elsewhere.

• Basic research in crashworthiness II - low speed impact tests of unmodified vehicles. Interim technical report. (1972), by K. N. Naab (page images at HathiTrust)
• Basic research in crashworthiness II - low speed impact tests of modified vehicles. Interim technical report. (1973), by K. N. Naab (page images at HathiTrust)
• Basic research in crashworthiness II - dynamic analysis of elasto-plastic space frame structures. Interim technical report. (1973), by C. Y. Sheu (page images at HathiTrust; US access only)
• Crash injury reduction and post-crash factors evaluations - Ford ESV's - forty-mph, fifty-mph, and low-speed barrier impacts. Final report. (1974) (page images at HathiTrust)
• Final design and implementation plan for evaluating the effectiveness of FMVSS 215: exterior protection. Tasks #4 & #5 report. (1977) (page images at HathiTrust)
• Damageability tests of Minicars' RSV. Final report. (1980), by R. Garn and S. Davis (page images at HathiTrust)
• Relationship of operating speeds to roadway geometric design speeds. (1996), by Christopher M. Poe, J. P. Tarris, and John M. Mason (page images at HathiTrust)
• High-lift characteristics of a variable-sweep supersonic transport model with a blended engine-fuselage and engine-mounted horizontal tails (National Aeronautics and Space Administration ;, 1966), by Vernard E. Lockwood and Langley Research Center (page images at HathiTrust)
• Wind-tunnel investigation of the aerodynamic characteristics of a model representative of a supersonic fighter-class airplane with an external-flow jet-augmented flap in low-speed flight (National Aeronautics and Space Administration, 1959), by William A. Newsom and Langley Research Center (page images at HathiTrust)
• Low-speed wind-tunnel investigation of a wingless jet VTOL transport model (National Aeronautics and Space Administration, 1959), by Marion O. McKinney and Langley Research Center (page images at HathiTrust)
• Flight test of a 30-foot nominal diameter disk-gap-band parachute deployed at a Mach number of 1.56 and a dynamic pressure of 11.4 pounds per square foot (National Aeronautics and Space Administration ;, 1967), by Clinton V. Eckstrom, John S. Preisser, and Langley Research Center (page images at HathiTrust)

Items below (if any) are from related and broader terms.