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Books by Development United States. Army. Missile Command. Research:

Books in the extended shelves:

• United States. Army. Missile Command. Research, Development, and Engineering Center: An assessment of the Martin-Marietta high angle of attack aerodynamic methodology for body tail missiles (Redstone Arsenal, Alabama ; U.S. Army Missile Command, Research, Development, and Engineering Laboratory, 1976., 1976), also by Donald J. Spring, Gary C. Winn, Jimmie N. Derrick, and Redstone Arsenal (Ala.) (page images at HathiTrust)
• United States. Army. Missile Command. Research, Development, and Engineering Center: The effect of wrap-around fins on aerodynamic stability and rolling moment variations (Redstone Arsenal, Alabama ; U.S. Army Missile Command, Research, Development, and Engineering Laboratory, 1973., 1973), also by C. W. Dahlke, J. C. Craft, and Redstone Arsenal (Ala.) (page images at HathiTrust)
• United States. Army. Missile Command. Research, Development, and Engineering Center: The effectiveness of canards for roll control. (Redstone Arsenal, Alabama ; U.S. Army Missile Command, Research, Development, and Engineering Laboratory, 1976., 1976), also by James R Burt and Redstone Arsenal (Ala.) (page images at HathiTrust)
• United States. Army. Missile Command. Research, Development, and Engineering Center: An experimental investigation of the aerodynamic characteristics of nose mounted canard configurations at supersonic Mach numbers (1.5 through 4.5) (Redstone Arsenal, Alabama ; U.S. Army Missile Command, Research, Development, and Engineering Laboratory, 1976., 1976), also by James R Burt, Redstone Arsenal (Ala.), and Chryler Corporation (page images at HathiTrust)
• United States. Army. Missile Command. Research, Development, and Engineering Center: An experimental investigation of the aerodynamic characteristics of several nose-mounted canard configurations at transonic Mach numbers (Redstone Arsenal, Alabama ; U.S. Army Missile Command, Research, Development, and Engineering Laboratory, 1974., 1974), also by James R Burt, Redstone Arsenal (Ala.), and Chrysler Corporation (page images at HathiTrust)
• United States. Army. Missile Command. Research, Development, and Engineering Center: An exploratory investigation on reducing supersonic missile drag by fluid injection into a turbulent boundary layer (Redstone Arsenal, Alabama ; U.S. Army Missile Command, Research, Development, and Engineering Laboratory, 1976., 1976), also by Donald Rubin and Redstone Arsenal (Ala.) (page images at HathiTrust)
• United States. Army. Missile Command. Research, Development, and Engineering Center: Investigation of jet plume effects on the longitudinal stability characteristics of a body of revolution with various fin configurations at Mach numbers from 0.2 to 2.3 : normal jet plume simulator (Redstone Arsenal, Alabama ; U.S. Army Missile Command, Research, Development, and Engineering Laboratory, 1976., 1976), also by James H. Henderson and Redstone Arsenal (Ala.) (page images at HathiTrust)
• United States. Army. Missile Command. Research, Development, and Engineering Center: An investigation of streamwise body-fin gaps as a means of alleviating the adverse plume effects on missile longitudinal stability. (Redstone Arsenal, Alabama ; U.S. Army Missile Command, Research, Development, and Engineering Laboratory, 1977., 1977), also by James H. Henderson and Redstone Arsenal (Ala.) (page images at HathiTrust)
• United States. Army. Missile Command. Research, Development, and Engineering Center: Inviscid flow analysis on body of revolution with slender cruciform canted delta fins at small angle of incidence (Redstone Arsenal, Alabama ; U.S. Army Missile Command, Research, Development, and Engineering Laboratory, 1975., 1975), also by N. Uchiyama, J. M. Wu, Redstone Arsenal (Ala.), and University of Tennessee (System). Space Institute (page images at HathiTrust)
• United States. Army. Missile Command. Research, Development, and Engineering Center: A summary of jet plume effects on the stability characteristics of a body of revolution with various fin configurations at Mach numbers from 0.2 to 2.3 : normal jet plume simulator (Redstone Arsenal, Alabama ; U.S. Army Missile Command, Research, Development, and Engineering Laboratory, 1976., 1976), also by George Batiuk, James H. Henderson, and Redstone Arsenal (Ala.) (page images at HathiTrust)
• United States. Army. Missile Command. Research, Development, and Engineering Center: Transonic wind tunnel investigation of thrust effects on the longitudinal stability characteristics of several body-fin configurations : sting-mounted model with normal-jet plume simulator (Redstone Arsenal, Alabama ; U.S. Army Missile Command, Research, Development, and Engineering Laboratory, 1974., 1974), also by James H. Henderson, Redstone Arsenal (Ala.), and Chrysler Corporation (page images at HathiTrust)

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