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Pressure And Static Force Test Of Three Elliptic Missile Body Configurations At Mach Numbers 15 To 50
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Book Synopsis Pressure and Static Force Test of Three Elliptic Missile Body Configurations at Mach Numbers 1.5 to 5.0 by : M. E. Sellers
Download or read book Pressure and Static Force Test of Three Elliptic Missile Body Configurations at Mach Numbers 1.5 to 5.0 written by M. E. Sellers and published by . This book was released on 1983 with total page 104 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Pressure and Static Force Test of Three Elliptic Missile Body Configurations at Mach Numbers 1.5 to 5.0 by : M. E. Sellers
Download or read book Pressure and Static Force Test of Three Elliptic Missile Body Configurations at Mach Numbers 1.5 to 5.0 written by M. E. Sellers and published by . This book was released on 1983 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Pressure Test of Three Elliptic Missile Body Configuratins by : Marvin E. Sellers
Download or read book Pressure Test of Three Elliptic Missile Body Configuratins written by Marvin E. Sellers and published by . This book was released on 1985 with total page 42 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Static Stability Test of Three Elliptic Missile Body Configurations by : Marvin E. Sellers
Download or read book Static Stability Test of Three Elliptic Missile Body Configurations written by Marvin E. Sellers and published by . This book was released on 1985 with total page 62 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Pressure Test of Three Elliptic Missile Body Configurations by : Marvin E. Sellers
Download or read book Pressure Test of Three Elliptic Missile Body Configurations written by Marvin E. Sellers and published by . This book was released on 1985 with total page 39 pages. Available in PDF, EPUB and Kindle. Book excerpt: A wind tunnel test was conducted to obtain the surface pressure distributions of three elliptic missile body configurations. The test was performed at nominal Mach numbers from 0.4 to 1.3 at a constant nominal free-stream unit Reynolds number of 2.4 million per ft. The angle-of-attack range was -4 to 20 deg at sideslip angles of -4, 0, and 4 deg. Only sample tabulations of the test results are included in the report. Keywords: Elliptic bodies, Power law bodies, Pressure test, Transonic flow.
Book Synopsis Static Stability Test of Three Elliptic Missile Body Configurations by :
Download or read book Static Stability Test of Three Elliptic Missile Body Configurations written by and published by . This book was released on 1985 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt: A wind tunnel test was conducted to obtain data on the aerodynamic characteristics of three elliptic missile body configurations. The test was performed at nominal Mach numbers from 0.4 to 1.3 at a constant nominal free-stream unit Reynolds number of 2.4 million per ft. The angle-of-attack range was -4 to 20 deg at sideslip angles of 0 and 4 deg. Only sample tabulations of the test results are included in the report.
Book Synopsis Investigation of the Static Longitudinal Stability and Roll Characteristics of a Three-stage Missile Configuration at Mach Numbers from 1.77 to 2.87 by : Donald T. Gregory
Download or read book Investigation of the Static Longitudinal Stability and Roll Characteristics of a Three-stage Missile Configuration at Mach Numbers from 1.77 to 2.87 written by Donald T. Gregory and published by . This book was released on 1959 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Static Stability and Drag Characteristics of the HAST Missile at Mach Numbers 2.25, 3.0, and 4.0 by : J. T. Best (Jr.)
Download or read book Static Stability and Drag Characteristics of the HAST Missile at Mach Numbers 2.25, 3.0, and 4.0 written by J. T. Best (Jr.) and published by . This book was released on 1974 with total page 194 pages. Available in PDF, EPUB and Kindle. Book excerpt: Static-force tests were conducted at Mach number 2.25, 3, and 4 on a 0.25 -scale model of the High Altitude Supersonic Target (HAST) missile.
Book Synopsis Scientific and Technical Aerospace Reports by :
Download or read book Scientific and Technical Aerospace Reports written by and published by . This book was released on 1980 with total page 794 pages. Available in PDF, EPUB and Kindle. Book excerpt: Lists citations with abstracts for aerospace related reports obtained from world wide sources and announces documents that have recently been entered into the NASA Scientific and Technical Information Database.
Book Synopsis Government-wide Index to Federal Research & Development Reports by :
Download or read book Government-wide Index to Federal Research & Development Reports written by and published by . This book was released on 1966-11 with total page 1080 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Wind Tunnel Tests of Elliptical Missile Body Configurations at Mach Numbers 0.4 to 5.0 by : Donald E. Shereda
Download or read book Wind Tunnel Tests of Elliptical Missile Body Configurations at Mach Numbers 0.4 to 5.0 written by Donald E. Shereda and published by . This book was released on 1987 with total page 161 pages. Available in PDF, EPUB and Kindle. Book excerpt: A large body of wind tunnel data was generated by tests of missile bodies of varying ellipticity ratios. The tests were conducted at subsonic through high supersonic speeds at angles of attack from -4 to 20 degrees. Measurements of both surface pressure and total forces and moments were made at a variety of Mach numbers and Reynolds number combinations. This data was supplemented with flow visualization data such as vapor screens, oil flows and shadowgraphs at selected supersonic Mach numbers. The missile bodies were power-law bodies with an exponent of 0.5 and ellipticity ratios of 2.0, 2.5, and 3.0 to 1. Comparisons of selected data with various prediction codes (Supersonic/Hypersonic Arbitrary Body Program, NSWC Euler Code, Missile Datcom, and FLO-57 Euler Code) were made. The test data provided insight into the effects of several variables and will provide a good data base for correlations with numerical techniques.
Book Synopsis Aerodynamic Characteristics in Pitch of Several Triple-body Missile Configurations at Mach Numbers 0.6 to 1.4 by : Earl D. Knechtel
Download or read book Aerodynamic Characteristics in Pitch of Several Triple-body Missile Configurations at Mach Numbers 0.6 to 1.4 written by Earl D. Knechtel and published by . This book was released on 1956 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt: An experimental investigation was conducted to determine the longitudinal aerodynamic characteristics at transonic speeds of missile configurations having three blunted cone-cylinder bodies. Modifications of the basic model were tested to indicate the effects of (a) relative lengths of coplanar bodies, (b) seals between the cylindrical portions of the bodies, (c) horizontal connecting surfaces near the rear of the bodies, and (d) triangular rather than coplanar body grouping. Lift, drag, and pitching-moment data were obtained at angles of attack from -4 to 12 degrees and Mach numbers from 0.6 to 1.4 for a constant Reynolds number of 5,500,000, based on average body length.
Book Synopsis Aerodynamic Test and Analysis of a Slender Generic Missile Configuration by : Roger S. Gates
Download or read book Aerodynamic Test and Analysis of a Slender Generic Missile Configuration written by Roger S. Gates and published by . This book was released on 1989 with total page 14 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Investigation of the Static Longitudinal Stability Characteristics of a Model of an Intermediate-range Ballistic Missile at Mach Numbers Between 1.57 and 4.65 by : Robert M. Lust
Download or read book Investigation of the Static Longitudinal Stability Characteristics of a Model of an Intermediate-range Ballistic Missile at Mach Numbers Between 1.57 and 4.65 written by Robert M. Lust and published by . This book was released on 1960 with total page 50 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Free-flight Investigation of the Static Stability and Aerodynamic Drag of Three Blunt- Nosed Cylinder-flare Test Bodies at Mach Numbers from 13 to 17 by :
Download or read book Free-flight Investigation of the Static Stability and Aerodynamic Drag of Three Blunt- Nosed Cylinder-flare Test Bodies at Mach Numbers from 13 to 17 written by and published by . This book was released on 1961 with total page 32 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Technical Abstract Bulletin written by and published by . This book was released on with total page 684 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Wind Tunnell Tests of Ellipical Missile Body Configurations at Mach Number 0.4 to 5.0 by : Donald E. Shereda
Download or read book Wind Tunnell Tests of Ellipical Missile Body Configurations at Mach Number 0.4 to 5.0 written by Donald E. Shereda and published by . This book was released on 1987 with total page 151 pages. Available in PDF, EPUB and Kindle. Book excerpt:
