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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 / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce, [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 /, 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 / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 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 / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 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 / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 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 / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [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 /, also by Edwin E.. Jr 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. / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [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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