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Books about United States. Army. Missile Command -- Books by United States. Army. Missile Command

Books about United States. Army. Missile Command:

Books by United States. Army. Missile Command:

Books in the extended shelves:

• United States. Army. Missile Command: Aerodynamic analysis of a "flex" fin concept (Redstone Arsenal, Alabama ; U.S. Army Missile Command, System Simulation and Development Directorate, Research, Development, and Enginering Center, 1987., 1987), also by George A. Sanders and Redstone Arsenal (Ala.) (page images at HathiTrust)
• United States. Army. Missile Command: Aerodynamic characteristics of a series of bodies with and without tails at Mach Numbers from 0.8 to 3.0 and angles of attack from 0 to 45 degrees (Redstone Arsenal, Alabama ; U.S. Army Missile Command, 1976., 1976), also by Jimmie N. Derrick, Gary C. Winn, Donald J. Spring, Redstone Arsenal (Ala.), and University of Tennessee (System). Space Institute (page images at HathiTrust)
• United States. Army. Missile Command: Aerodynamic characteristics of wraparound fins mounted on bodies of revolution and rheir influence on the missile static stability at Mach numbers from 0.3 to 1.3 (Redstone Arsenal, Alabama ; U.S. Army Missile Command, 1972., 1972), also by Calvin Wayne Dahlke, Joseph C. Craft, and Redstone Arsenal (Ala.) (page images at HathiTrust)
• United States. Army. Missile Command: Aerodynamic Data Base User's Guide (Redstone Arsenal, Alabama ; U.S. Army Missile Research and Development Command, Systems Simulation Directorate, Technology Laboratory, 1979., 1979), also by George M. Landingham and Redstone Arsenal (Ala.) (page images at HathiTrust)
• United States. Army. Missile Command: Aerodynamic performance of missile configurations at transonic speeds including the effects of a jet plume (Redstone Arsenal, Alabama : U.S. Army Missile Command, 1976., 1976), also by Jain-Ming Wu, U. Uchiyama, Trevor H. Moulden, Redstone Arsenal (Ala.), and University of Tennessee (System). Space Institute (page images at HathiTrust)
• United States. Army. Missile Command: Aerodynamic prediction methods, RDF-129 (Redstone Arsenal, Alabama ; U.S. Army Missile Command, Systems Simulation and Development Directorate, Research, Development, and Engineering Center, 1989., 1989), also by J. L. Sims, Robert H. Carnesi, L. G. Mendel, John F. Stalnaker, Redstone Arsenal (Ala.), and Georgia Tech Research Institute (page images at HathiTrust)
• United States. Army. Missile Command: Aerodynamics of longitudinally supported ring tail configurations (Redstone Arsenal, Alabama ; U.S. Army Missile Command, Aeroballistics Directorate, 1971., 1971), also by Calvin Wayne Dahlke and Redstone Arsenal (Ala.) (page images at HathiTrust)
• United States. Army. Missile Command: An approach to experimental investigation of jet plume effects on missile aerodynamics (Redstone Arsenal, Alabama ; U.S. Army Missile Command, Systems Simulation and Development Directorte, 1982., 1982), also by George M. Landingham and Redstone Arsenal (Ala.) (page images at HathiTrust)
• United States. Army. Missile Command: Approximate determination of jet contours near the exit of axially symmetrical nozzles as a basis for plume modeling (Redstone Arsenal, Alabama ; U.S. Army Missile Command, Directorate for Research, Development, Enginering and Missile Systems Laboratory, 1972., 1972), also by H. H. Korst and Redstone Arsenal (Ala.) (page images at HathiTrust)
• United States. Army. Missile Command: Computer program for estimating stability derivatives of missile configurations (Redstone Arsenal, Alabama ; U.S. Army Missile Command, 1976., 1976), also by William D. Washington and Redstone Arsenal (Ala.) (page images at HathiTrust)
• United States. Army. Missile Command: Computer program for estimating stability derivatives of missile configurations : users manual (Redstone Arsenal, Alabama ; U.S. Army Missile Command, Systems Simulation and Development Directorte, 1982., 1982), also by George A. Sanders and Redstone Arsenal (Ala.) (page images at HathiTrust)
• United States. Army. Missile Command: CRAFT time dependent analysis of a missile with lateral control jet (Redstone Arsenal, Alabama ; U.S. Army Missile Command, Systems Simulation and Development Directorate, Research, Development, and Engineering Center, 1992, 1992), also by Ashvin Hosangadi, Brian J. York, Redstone Arsenal (Ala.), and Science Applications International Corporation (page images at HathiTrust)
• United States. Army. Missile Command: Effect of forebody wing strakes on enhancing performance of a typical body-wing-tail missile configuration at Mach 2.0 (Redstone Arsenal, Alabama ; U.S. Army Missile Command, Systems Simulation and Development Directorte, 1980., 1980), also by Pamela K. Alstott, William David Washington, and Redstone Arsenal (Ala.) (page images at HathiTrust)
• United States. Army. Missile Command: Effect of missile nose length and shape on fin effectiveness (Redstone Arsenal, Alabama ; U.S. Army Missile Command, Advanced Systems Laboratory, Research and Engineering Directorate, 1970., 1970), also by Donald V. Rubin, Wiley Pettis, and Redstone Arsenal (Ala.) (page images at HathiTrust)
• United States. Army. Missile Command: An experimental investigation of a transverse jet ejecting from a flat plate into a subsonic free stream (Redstone Arsenal, Alabama ; U.S. Army Missile Command, Advanced Systems Laboratory, Research and Engineering Directorate, 1970., 1970), also by Troy A. Street and Redstone Arsenal (Ala.) (page images at HathiTrust)
• United States. Army. Missile Command: An experimental investigation of base pressure on a body of revolution at high thrust levels and free stream Mach numbers of 1.5 to 2.87 (Redstone Arsenal, Alabama ; U.S. Army Missile Command, Advanced Systems Laboratory, Research and Engineering Directorate, 1970., 1970), also by Joseph C. Craft, Charles E. Brazzel, and Redstone Arsenal (Ala.) (page images at HathiTrust)
• United States. Army. Missile Command: An experimental investigation of downstream flow-field properties behind a forward located sonic jet injected into transonic freestream from a body of revolution (Redstone Arsenal, Alabama ; U.S. Army Missile Command, Advanced Systems Laboratory, Research and Engineering Directorate, 1968., 1968), also by Calvin Wayne Dahlke and Redstone Arsenal (Ala.) (page images at HathiTrust)
• United States. Army. Missile Command: An experimental investigation of downstream flow-field properties behind a sonic jet injected into transonic free stream from a body of revolution : Series II (Redstone Arsenal, Alabama ; U.S. Army Missile Command, Advanced Systems Laboratory, Research and Engineering Directorate, 1969., 1969), also by Calvin Wayne Dahlke and Redstone Arsenal (Ala.) (page images at HathiTrust)
• United States. Army. Missile Command: An experimental investigation of the interference effects due to a lateral jet issuing from a body of revolution over the Mach number range of 0.8 to 4.5 (Redstone Arsenal, Alabama ; U.S. Army Missile Command, 1968., 1968), also by Donald J. Spring and Redstone Arsenal (Ala.) (page images at HathiTrust)
• United States. Army. Missile Command: An experimental investigation using a normal jet plume simulator to determine jet plume effects on a long slender rocket configuration at Mach numbers from 0.2 to 1.5 (Redstone Arsenal, Alabama ; U.S. Army Missile Research and Development Command, 1977., 1977), also by James H Henderson, G. Batiuk, Calvin Wayne Dahlke, and Redstone Arsenal (Ala.) (page images at HathiTrust)
• United States. Army. Missile Command: Experimental study on high subsonic turbulent flow incipient separation (Redstone Arsenal, Alabama ; U.S. Army Missile Command, 1976., 1976), also by Jain-Ming Wu, Hideki Kuwano, Redstone Arsenal (Ala.), and University of Tennessee (System). Space Institute (page images at HathiTrust)
• United States. Army. Missile Command: Free air plume overpressure for 2.75 inch rocket motors Mark 40 and Mark 66 (Redstone Arsenal, Alabama ; U.S. Army Missile Command, Ground Equipment and Missile Structures Directorate, 1980., 1980), also by Robert Bergman, Donald Davis, and Redstone Arsenal (Ala.) (page images at HathiTrust)
• United States. Army. Missile Command: Grid fin analysis. Vol. 1 (Redstone Arsenal, Alabama ; U.S. Army Missile Command, Systems Simulation and Development Directorate, Research, Development, and Engineering Center, 1994, 1994), also by John E. Burkhalter, Todd Michael Leleux, Redstone Arsenal (Ala.), and Auburn University (page images at HathiTrust)
• United States. Army. Missile Command: Guide to the operation of the MIRADCOM/UTSI computer program for plume induced sepertion at transonic speeds (Redstone Arsenal, Alabama ; U.S. Army Missile Research and Development Command, Aeroballistics Directorate, Technology Laboratory, 1977., 1977), also by D. J. Spring, Trevor H. Moulden, Redstone Arsenal (Ala.), and University of Tennessee (System). Space Institute (page images at HathiTrust)
• United States. Army. Missile Command: An investigation of flow and stability characteristics for a body of revolution with fins and flare in presence of Plume induced separation at Mach numbers 0.7 to 1.4 (Redstone Arsenal, Alabama ; U.S. Army Missile Research and Development Command, Aeroballistics Direcorate, Technology Laboratory, 1977., 1977), also by Calvin Wayne Dahlke and Redstone Arsenal (Ala.) (page images at HathiTrust)
• United States. Army. Missile Command: An investigation of jet plume effects on the stability characteristics of a body of revolution in conjunction with fins of various geometry and longitudinal positions at transonic speeds (sting-mounted model with normal jet plume simulator) (Redstone Arsenal, Alabama ; U.S. Army Missile Command, 1975., 1975), also by James H Henderson and Redstone Arsenal (Ala.) (page images at HathiTrust)
• United States. Army. Missile Command: Investigation of plume induced separation on a full-size missile at supersonic velocities (Redstone Arsenal, Alabama ; U.S. Army Missile Command, Systems Simulation and Development Directorte, 1980., 1980), also by T. A. Martin and Redstone Arsenal (Ala.) (page images at HathiTrust)
• United States. Army. Missile Command: An investigation of the aerodynamic stabilizing effectiveness of several split flare afterbody configurations in the presence of an underexpanded jet plume at transonic Mach numbers (Redstone Arsenal, Alabama ; U.S. Army Missile Research and Development Command, Aeroballistics Directorate, Technology Laboratory, 1978., 1978), also by James R. Burt and Redstone Arsenal (Ala.) (page images at HathiTrust)
• United States. Army. Missile Command: An investigation of the effectiveness of several devices in simulating a rocket plume at free stream Mach numbers 0.9 to 1.2 (Redstone Arsenal, Alabama ; U.S. Army Missile Command, 1971., 1971), also by James Robert Burt and Redstone Arsenal (Ala.) (page images at HathiTrust)
• United States. Army. Missile Command: Jet interaction control effectiveness for subsonic and supersonic flight : final report (Redstone Arsenal, Alabama ; U.S. Army Missile Command, 1969., 1969), also by Louis A. Cassel, James M. Kelso, Clark W. Bullard, Norbert A. Durando, Redstone Arsenal (Ala.), and McDonnell Douglas Astronautics Company-West (page images at HathiTrust)
• United States. Army. Missile Command: Missile dynamics equations for guidance and control modeling and analysis (Redstone Arsenal, Alabama : U.S. Army Missile Command, 1984., 1984), also by Philip N. Jenkins and Redstone Arsenal (Ala.) (page images at HathiTrust)
• United States. Army. Missile Command: Modified Barrowman Method with applications to the Optical Deep Attack Missile Systems and Precision Deep Attack Missile Systems vehicles (Redstone Arsenal, Alabama ; U.S. Army Missile Command, Research Directorate, Research, Development, and Enginering Center, 1989., 1989), also by Charles E. Hall and Redstone Arsenal (Ala.) (page images at HathiTrust)
• United States. Army. Missile Command: An outline of methods applicable to viscous fluid flow problems (Redstone Arsenal, Alabama ; U.S. Army Missile Command, 1971., 1971), also by Trevor H. Moulden, Jain-Ming Wu, Redstone Arsenal (Ala.), and University of Tennessee (System). Space Institute (page images at HathiTrust)
• United States. Army. Missile Command: Preliminary review of approximate calculative methods for transonic flow around bodies of revolution (Redstone Arsenal, Alabama ; U.S. Army Missile Command, 1972., 1972), also by Jain-Ming Wu, Kinya Aoyama, Redstone Arsenal (Ala.), and University of Tennessee (System). Space Institute (page images at HathiTrust)
• United States. Army. Missile Command: Pressure distributions for axisymmetric bodies with discontinuous curvature in transonic flow (Redstone Arsenal, Alabama ; U.S. Army Missile Command, 1970., 1970), also by Jain-Ming Wu, Kinya Aoyama, Redstone Arsenal (Ala.), and University of Tennessee (System). Space Institute (page images at HathiTrust)
• United States. Army. Missile Command: Solution of transient heat transfer problems for flat plates, cylinders, and spheres by finite-difference methods (Redstone Arsenal, Alabama ; U.S. Army Missile Command, Directorte of Research and Development, 1965., 1965), also by W. G. Burleson, R Eppes, and Redstone Arsenal (Ala.) (page images at HathiTrust)
• United States. Army. Missile Command: Static aerodynamic stability characteristics of a body of revolution with wraparound fins at Mach numbers from 0.5 to 1.3 (Redstone Arsenal, Alabama ; U.S. Army Missile Command, Advanced Systems Laboratory, Research and Engineering Directorate, 1972., 1972), also by John E. Vaughn, Calvin Wayne Dahlke, Joseph C. Craft, and Redstone Arsenal (Ala.) (page images at HathiTrust)
• United States. Army. Missile Command: Static aerodynamic stability characteristics of a body of revolution with wraparound fins at Mach numbers from 1.6 to 2.86 (Redstone Arsenal, Alabama ; U.S. Army Missile Command, 1972., 1972), also by John E. Vaughn, Calvin Wayne Dahlke, Joseph C. Craft, and Redstone Arsenal (Ala.) (page images at HathiTrust)
• United States. Army. Missile Command: A study of various slender and non-slender fin-body combinations of missile configurations (Redstone Arsenal, Alabama ; U.S. Army Missile Command, 1976., 1976), also by N. Uchiyama, Jain-Ming Wu, Redstone Arsenal (Ala.), and University of Tennessee (System). Space Institute (page images at HathiTrust)
• United States. Army. Missile Command: A study to determine the accuracy of two computer programs in predicting hinge moments for all movable tail fins on missile bodies (Redstone Arsenal, Alabama ; U.S. Army Missile Command, Systems Simulation and Development Directorte, 1983., 1983), also by George A. Sanders and Redstone Arsenal (Ala.) (page images at HathiTrust)
• United States. Army. Missile Command: A summary of aerodynamic characteristics for wrap-around fins from Mach 0.3 to 3.0 (Redstone Arsenal, Alabama ; U.S. Army Missile Research and Development Command, 1977., 1977), also by James A. Humphrey, Calvin Wayne Dahlke, and Redstone Arsenal (Ala.) (page images at HathiTrust)
• United States. Army. Missile Command: Supersonic flow around right circular cones, tables for zero angle of attack (Redstone Arsenal, Alabama ; U.S. Army Ballistic Missile Agency, Aerodynamics Analysis Branch, Aeroballistics Laboratory, 1960., 1960), also by Joseph L. Sims and Redstone Arsenal (Ala.) (page images at HathiTrust)
• United States. Army. Missile Command: Technical facilities and capabilities. (Redstone Arsenal, Ala., 1963) (page images at HathiTrust)
• United States. Army. Missile Command: Theoretical analysis of the flow field over a family of ogive bodies (Redstone Arsenal, Alabama ; U.S. Army Missile Research and Development Command, Aeroballistics Directorate, 1977., 1977), also by Ronnie W. Guy, Redstone Arsenal (Ala.), and inc Science Applications (page images at HathiTrust)
• United States. Army. Missile Command: Theoretical analysis of the flow field over a family of ogive bodies : a supplement to MIRADCOM technical report TD-CR-77-5I (Redstone Arsenal, Alabama ; U.S. Army Missile Research and Development Command, Systems Simulation Directorate, Technology Laboratory, 1979., 1979), also by R. L. Richardson, B. Z. Jenkins, and Redstone Arsenal (Ala.) (page images at HathiTrust)
• United States. Army. Missile Command: Theoretical analysis of the flow field over a family of ogive bodies. Volume II (Redstone Arsenal, Alabama ; U.S. Army Missile Command, Technology Laboratory, 1979., 1979), also by R. L. Richardson, B. Z. Jenkins, and Redstone Arsenal (Ala.) (page images at HathiTrust)
• United States. Army. Missile Command: Thrust effects on missile aerodynamics (Redstone Arsenal, Alabama ; U.S. Army Missile Command, Directorate for Research, Development, Enginering and Missile Systems Laboratory, 1971., 1971), also by R. A. Deep, C. E. Brazzel, James H. Henderson, and Redstone Arsenal (Ala.) (page images at HathiTrust)
• United States. Army. Missile Command: Transonic flow-field calculation around ogive cylinders by nonlinear-linear stretching method (Redstone Arsenal, Alabama ; U.S. Army Missile Command, 1970., 1970), also by Jain-Ming Wu, Kinya Aoyama, Redstone Arsenal (Ala.), and University of Tennessee (System). Space Institute (page images at HathiTrust)
• United States. Army. Missile Command: Transonic flow fields around various bodies of revolution including preliminary studies on viscous effects with and without plume : summary report (Redstone Arsenal, Alabama ; U.S. Army Missile Command, 1971., 1971), also by Jain-Ming Wu, Trevor H. Moulden, Kinya Aoyama, Redstone Arsenal (Ala.), and University of Tennessee (System). Space Institute (page images at HathiTrust)
• United States. Army. Missile Command: User's manual for the Martin-Marietta high angle of attack aerodynamic methodology for body tail missiles (Redstone Arsenal, Alabama ; U.S. Army Missile Research and Development Command, Aeroballistics Directorate, Technology Laboratory, 1978., 1978), also by Gary C. Winn and Redstone Arsenal (Ala.) (page images at HathiTrust)

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