The Online Books Page

Books by Francis J. Capone:

Books in the extended shelves:

• Capone, Francis J.: Aerodynamic characteristics of a supersonic fighter aircraft model at Mach 0.40 to 2.47 (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1986), also by Dorothy Arbiter, E. Ann Bare, and Langley Research Center (page images at HathiTrust)
• Capone, Francis J.: Aeropropulsive characteristics of canted twin pitch-vectoring nozzles at Mach 0.20 to 1.20 (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1991), also by Mary L. Mason and Langley Research Center (page images at HathiTrust)
• Capone, Francis J.: Aeropropulsive characteristics of nonaxisymmetric-nozzle thrust reversers at Mach numbers from 0 to 1.20 (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1984), also by George T. Carson, Mary L. Mason, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Capone, Francis J.: Aeropropulsive characteristics of twin nonaxisymmetric vectoring nozzles installed with forward swept and aft-swept wings (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), also by United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Capone, Francis J.: Aeropropulsive characteristics of twin single-expansion-ramp vectoring nozzles installed with forward-swept wings and canards (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1983), also by Mary L. Mason and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Capone, Francis J.: Aeropulsive characteristics at Mach numbers up to 2.2 of axisymmetric and nonaxisymmetric nozzles installed on an F-18 model (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1982), also by Langley Research Center and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Capone, Francis J.: Effect of in-flight thrust reversing on vertical-tail loads of F-18 and F-15 airplane models (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), also by E. Ann Bare, Bobby L. Berrier, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Capone, Francis J.: Effect of port corner geometry on the internal performance of a rotating-vane-type thrust reverser (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1986), also by Bobby L. Berrier and Langley Research Center (page images at HathiTrust)
• Capone, Francis J.: Effect of thrust vectoring and wing maneuver devices on transonic aeropropulsive characteristics of a supersonic fighter aircraft (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1983), also by David E. Reubush and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Capone, Francis J.: Effects of nozzle exit location and shape on propulsion-induced aerodynamic characteristics due to vectoring twin nozzles at Mach numbers from 0.4 ̥to 1.2 (U.S. National Aeronautics and Space Administration ;, 1976), also by Langley Research Center (page images at HathiTrust)
• Capone, Francis J.: Effects of varying podded nacelle-nozzle installations on transonic aeropropulsive characteristics of a supersonic fighter aircraft (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1983), also by David E. Reubush and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Capone, Francis J.: The effects on propulsion-induced aerodynamic forces of vectoring a partial-span rectangular jet at Mach numbers from 0.40 to 1.20 (National Aeronautics and Space Administration ;, 1975), also by Langley Research Center (page images at HathiTrust)
• Capone, Francis J.: An experimental investigation of thrust vectoring two-dimensional covergent-divergent nozzles installed in a twin-engine fighter model at high angles of attack (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1990), also by Laurence D. Leavitt, Mary L. Mason, and Langley Research Center (page images at HathiTrust)
• Capone, Francis J.: An investigation of a close-coupled canard as a direct side-force generator on a fighter model at Mach numbers from 0.40 to 0.90 (National Aeronautics and Space Administration ;, 1977), also by Richard J. Re, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Capone, Francis J.: Investigation of Axisymmetric and nonaxisymmetric nozzels installed on a 0.10-scale F-18 protype airplane model (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1980), also by Bobby L. Berrier, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Capone, Francis J.: Longitudinal aerodynamic characteristics of a fighter model with a close-coupled canard at Mach numbers from 0.40 to 1.20 (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), also by Richard J. Re and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Capone, Francis J.: Multiaxis control power from thrust vectoring for a supersonic fighter aircraft model at Mach 0.20 to 2.47 (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1987), also by E. Ann Bare and Langley Research Center (page images at HathiTrust)
• Capone, Francis J.: NASA TN D-5314 (National Aeronautics and Space Administration ;, 1969), also by Harry T. Norton, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Capone, Francis J.: NASA TN D-5316 (National Aeronautics and Space Administration ;, 1969), also by Langley Research Center and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Capone, Francis J.: NASA TN D-5553 (National Aeronautics and Space Administration ; [For sale for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1969), also by Lawrence E. Putnam, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Capone, Francis J.: NASA TN D-5971 (National Aeronautics and Space Administration :, 1970), also by Langley Research Center and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Capone, Francis J.: Performance of twin two-dimensional wedge nozzles including thrust vectoring and reversing effects at speeds up to Mach 2.20 (National Aeronautics and Space Administration ;, 1977), also by Donald L. Maiden, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
• Capone, Francis J.: Static internal performance of an axisymmetric nozzle with multiaxis thrust-vectoring capability (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1991), also by George T. Carson and Langley Research Center (page images at HathiTrust)
• Capone, Francis J.: Static internal performance of convergent single-expansion-ramp nozzles with various combinations of internal geometric parameters (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1989), also by E. Ann Bare (page images at HathiTrust)
• Capone, Francis J.: A static investigation of the thrust vectoring system of the F/A-18 high-alpha research vehicle (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992), also by Mary L. Mason, Scott C. Asbury, and Langley Research Center (page images at HathiTrust)
• Capone, Francis J.: Static performance of five twin-engine nonaxisymmetric nozzles with vectoring and reversing capability (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), also by United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Capone, Francis J.: Transonic wind-tunnel tests of an error-compensated static-pressure probe (National Aeronautics and Space Administration, 1961), also by United States National Aeronautics and Space Administration and Langley Research Center (page images at HathiTrust)
• Capone, Francis J.: Wind-tunnel tests of seven static-pressure probes at transonic speeds (National Aeronautics and Space Administration, 1961), also by United States National Aeronautics and Space Administration and Langley Research Center (page images at HathiTrust)

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