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Runckel, Jack F.: Investigation of Catalyst Beds for 98-Percent-Concentration Hydrogen Peroxide (NASA Technical Note D-1808; Washington: National Aeronautics and Space Administration, 1963), also by Conrad M. Willis and Leland B. Salters (page images at HathiTrust)Help with reading books -- Report a bad link -- Suggest a new listing
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Runckel, Jack F.: Aerodynamic load measurements and opening characteristics of automatic leading-edge slats on a 45 degree sweptback wing at transonic speeds (National Aeronautics and Space Administration :, 1961), also by Donald D. Arabian, Charles F. Reid, and United States National Aeronautics and Space Administration (page images at HathiTrust) Runckel, Jack F.: Aerodynamic load measurements and opening characteristics of automatic leading-edge slats on a 45° sweptback wing at transonic speeds (Washington, D.C. : National Advisory Committee for Aeronautics, 1954., 1954), also by Donald D. Arabian, Charles F. Reid, Langley Aeronautical Laboratory, and United States National Advisory Committee for Aeronautics (page images at HathiTrust) Runckel, Jack F.: Calibration of the Langley 16-foot transonic tunnel with test section air removal (National Aeronautics and Space Administration ;, 1974), also by Blake W. Corson, William B. Igoe, and Langley Research Center (page images at HathiTrust) Runckel, Jack F.: Effect of fineness ratio on boattail drag of circular-arc afterbodies having closure ratios of 0.50 with jet exhaust at Mach numbers up to 1.30 (National Aeronautics and Space Administration ;, 1973), also by David E. Reubush and Langley Research Center (page images at HathiTrust) Runckel, Jack F.: Interference between exhaust system and afterbody of twin-engine fuselage configurations (National Aeronautics and Space Administration ;, 1974), also by Langley Research Center (page images at HathiTrust) Runckel, Jack F.: Investigation at transonic speeds of the loading over a 40 degree sweptback wing having an aspect ratio of 3, a taper ratio of 0.2 and NACA 65A004 airfoil sections (National Aeronautics and Space Administration :, 1961), also by United States National Aeronautics and Space Administration (page images at HathiTrust) Runckel, Jack F.: Investigation at transonic speeds of the loading over a 45 degree sweptback wing having an aspect ratio of 3, a taper ratio of 0.2, and NACA 65A004 airfoil sections (Washington, D.C. : National Advisory Committee for Aeronautics, [1956], 1956), also by Edwin E.. Lee, Langley Aeronautical Laboratory, and United States National Advisory Committee for Aeronautics (page images at HathiTrust) Runckel, Jack F.: Normal-force and hinge-moment characteristics at transonic speeds of flap-type ailerons at three spanwise locations on a 4-percent-thick sweptback-wing-body model and pressure-distribution measurements on an inboard aileron. (National Aeronautics and Space Administration :, 1961), also by Gerald Hieser and United States National Aeronautics and Space Administration (page images at HathiTrust)See also what's at your library, or elsewhere.
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