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Army Research and Technology Laboratories (U.S.). Structures Laboratory

Books from the extended shelves:

• Army Research and Technology Laboratories (U.S.). Structures Laboratory: Aerodynamic characteristics of three helicopter rotor airfoil sections at Reynolds numbers from model scale to full scale at Mach numbers from 0.35 to 0.90 (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1980), also by Kevin W. Noonan, Gene J. Bingham, United States. Army Aviation Research and Development Command, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Army Research and Technology Laboratories (U.S.). Structures Laboratory: Analysis of stability contributions of high dihedral V-trails (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), also by Carl F. Freeman, William T. Yeager, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Army Research and Technology Laboratories (U.S.). Structures Laboratory: Computer program for generating input for analysis of impingement-cooled, axial-flow turbine blade (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1980), also by David Rosenbaum, Lewis Research Center, Propulsion Laboratory (U.S.), and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Army Research and Technology Laboratories (U.S.). Structures Laboratory: Coupled rotor/airframe vibration analysis (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1982), also by Robert Sopher, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, United Technologies Corporation. Sikorsky Aircraft Division, and Langley Research Center (page images at HathiTrust)
• Army Research and Technology Laboratories (U.S.). Structures Laboratory: Development and validation of a combined rotor-fuselage induced flow-field computational method (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1980), also by Carl E. Freeman, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Army Research and Technology Laboratories (U.S.). Structures Laboratory: Effect of display size on utilization of traffic situation display for self-spacing task (National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1981), also by Terence S. Abbott, Gene C. Moen, and Lewis Research Center (page images at HathiTrust)
• Army Research and Technology Laboratories (U.S.). Structures Laboratory: Effects of static tensile load on the thermal expansion of Gr/PI composite material (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), also by Gary L. Farley and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Army Research and Technology Laboratories (U.S.). Structures Laboratory: Evaluation of helicopter noise due to blade-vortex interaction for five tip configurations (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1979), also by Danny R. Hoad, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Army Research and Technology Laboratories (U.S.). Structures Laboratory: Experimental investigation of effects of blade tip geometry on loads and performance for an articulated rotor system (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1979), also by William H. Weller and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Army Research and Technology Laboratories (U.S.). Structures Laboratory: Experimental investigation of three helicopter rotor airfoils designed analytically (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1979), also by Gene J. Bingham, Kevin W. Noonan, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Army Research and Technology Laboratories (U.S.). Structures Laboratory: Flight investigation of cockpit-displayed traffic information utilizing coded symbology in an advanced operational environment (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1980), also by Terence S. Abbott, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Army Research and Technology Laboratories (U.S.). Structures Laboratory: An improved computational procedure for determining helicopter rotor blade natural modes (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), also by William H. Weller, Raymond E. Mineck, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Army Research and Technology Laboratories (U.S.). Structures Laboratory: A laser velocimeter flow survey above a stalled wing (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), also by Warren H. Young, Danny R. Hoad, James F. Meyers, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Army Research and Technology Laboratories (U.S.). Structures Laboratory: Low-speed aerodynamic characteristics of a 16-percent thick variable-geometry airfoil designed for general aviation applications (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), also by Richard W. Barnwell, Robert J. McGhee, Kevin W. Noonan, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Army Research and Technology Laboratories (U.S.). Structures Laboratory: Performance testing of a main rotor system for a utility helicopter at 1/4 scale (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1982), also by John D. Berry and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Army Research and Technology Laboratories (U.S.). Structures Laboratory: Preliminary rotor wake measurements with a laser velocimeter (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1983), also by Danny R. Hoad, David B. Rhodes, James F. Meyers, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Army Research and Technology Laboratories (U.S.). Structures Laboratory: Reduction of high-speed impulsive noise by blade planform modification of a model helicopter rotor (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1982), also by David A. Conner, Danny R. Hoad, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Army Research and Technology Laboratories (U.S.). Structures Laboratory: Rotorcraft blade mode damping identification from random responses using a recursive maximum likelihood algorithm (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1982), also by John A. Molusis, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and Langley Research Center (page images at HathiTrust)
• Army Research and Technology Laboratories (U.S.). Structures Laboratory: Simulation study of traffic-sensor noise effects on utilization of traffic situation display for self-spacing task (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1983), also by David H. Williams, Gene C. Moen, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Army Research and Technology Laboratories (U.S.). Structures Laboratory: Wind-tunnel investigation of an armed mini remotely piloted vehicle (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1979), also by Arthur E. Phelps and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Army Research and Technology Laboratories (U.S.). Structures Laboratory: Wind-tunnel investigation of the effects of blade tip geometry on the interaction of torsional loads and performance for an articulated helicopter rotor (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), also by William T. Yeager, Wayne R. Mantay, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Army Research and Technology Laboratories (U.S.). Structures Laboratory: Wind-tunnel test of an articlulated helicopter rotor model with several tip shapes (National Aeronautics and Space Administrat ion, Scientific and Technical Information Branch ;, 1980), also by John D. Berry, Raymond E. Mineck, United States. Army Aviation Research and Development Command, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)

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