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Aerodynamic Characteristics In Pitch Of A 1 7 Scale Model Of A Two And Three Stage Rocket Configuration At Mach Numbers Of 04 To 463
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Book Synopsis Aerodynamic Characteristics in Pitch of a 1/7-scale Model of a Two- and Three-stage Rocket Configuration at Mach Numbers of 0.4 to 4.63 by : William F. Hinson
Download or read book Aerodynamic Characteristics in Pitch of a 1/7-scale Model of a Two- and Three-stage Rocket Configuration at Mach Numbers of 0.4 to 4.63 written by William F. Hinson and published by . This book was released on 1969 with total page 52 pages. Available in PDF, EPUB and Kindle. Book excerpt: Aerodynamic characteristics in pitch of scale model of two and three stage rocket configuration at Mach numbers of 0.4 to 4.63.
Book Synopsis Aerodynamic Characteristics in Pitch of a 1/7-scale Model of a Two- and Three-stage Rocket Configuration at Mach Numbers of 0.4 to 4.63 by : William F. Hinson
Download or read book Aerodynamic Characteristics in Pitch of a 1/7-scale Model of a Two- and Three-stage Rocket Configuration at Mach Numbers of 0.4 to 4.63 written by William F. Hinson and published by . This book was released on 1969 with total page 40 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Static Aerodynamic Characteristics of a Two-stage and a Three-stage Rocket Vehicle at Mach Numbers from 1.47 to 4.63 by : Clarence A. Brown
Download or read book Static Aerodynamic Characteristics of a Two-stage and a Three-stage Rocket Vehicle at Mach Numbers from 1.47 to 4.63 written by Clarence A. Brown and published by . This book was released on 1962 with total page 86 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Static Aerodynamic Characteristics of Three Rocket-vehicle Configurations at Mach Numbers from 1.80 to 4.63 Including Some Effects of Fin Size, Fin Cant, and Auxiliary Rocket Motors by : Dennis E. Fuller
Download or read book Static Aerodynamic Characteristics of Three Rocket-vehicle Configurations at Mach Numbers from 1.80 to 4.63 Including Some Effects of Fin Size, Fin Cant, and Auxiliary Rocket Motors written by Dennis E. Fuller and published by . This book was released on 1963 with total page 64 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Effects of Body and Fin Deflections on the Aerodynamic Characteristics in Pitch of a 0.065-scale Model of a Four-stage Rocket Configuration at Mach Numbers of 1.41 and 1.82 by : Ross B. Robinson
Download or read book Effects of Body and Fin Deflections on the Aerodynamic Characteristics in Pitch of a 0.065-scale Model of a Four-stage Rocket Configuration at Mach Numbers of 1.41 and 1.82 written by Ross B. Robinson and published by . This book was released on 1959 with total page 38 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Static Aerodynamic Characteristics of a Two-stage and a Three-stage Rocket Vehicle at Mach Numbers from 1.47 to 4.63 by : CLARENCE A. JR. BROWN
Download or read book Static Aerodynamic Characteristics of a Two-stage and a Three-stage Rocket Vehicle at Mach Numbers from 1.47 to 4.63 written by CLARENCE A. JR. BROWN and published by . This book was released on 1962 with total page 1 pages. Available in PDF, EPUB and Kindle. Book excerpt: An investigation was conducted in the Langley Unitary Plan wind tunnel to determine the effects of fin cant and size on the static aerodynamic characteristics of a 0.081-scale model of a three-stage and a two-stage Trailblazer II configuration. Tests were performed at Mach numbers from 1.47 to 4.63 and at a Reynolds number per foot of 3.0 x 10 to the 6th power. he angleof-attack range varied from approximately -5 to 5 degrees and angle of sideslip varied from approximately -4 to 4 degrees. All first-stage fins tested gave adequate static stability when the center-of-gravity travel of the flight model was taken into account. The presence of the auxiliary rocket motors in the lateral plane decreased the effectiveness of the fins in the pitch plane at the lower Mach number and increased the fin effectiveness at the higher Mach numbers. Removal of the auxiliary rocket motors from the first stage of the two-stage configuration reduced the axial force about 25% at the low Mach numbers and about 15% at the high Mach numbers. (Author).
Book Synopsis Aerodynamic Characteristics in Pitch and Sideslip of a 1/15-scale Model of the Scout Vehicle at a Mach Number of 2.01 by : Ross B. Robinson
Download or read book Aerodynamic Characteristics in Pitch and Sideslip of a 1/15-scale Model of the Scout Vehicle at a Mach Number of 2.01 written by Ross B. Robinson and published by . This book was released on 1961 with total page 42 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Aerodynamic Loading Characteristics of a 1/10-scale Model of the Three-stage Scout Vehicle at Mach Numbers 1.57 to 4.65 by : Lloyd S. Jernell
Download or read book Aerodynamic Loading Characteristics of a 1/10-scale Model of the Three-stage Scout Vehicle at Mach Numbers 1.57 to 4.65 written by Lloyd S. Jernell and published by . This book was released on 1963 with total page 52 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Investigation of the Aerodynamic Characteristics of Two Preliminary Designs of Scout Research Vehicle at Mach Numbers from 1.77 to 4.65 by : Robert J. Keynton
Download or read book Investigation of the Aerodynamic Characteristics of Two Preliminary Designs of Scout Research Vehicle at Mach Numbers from 1.77 to 4.65 written by Robert J. Keynton and published by . This book was released on 1961 with total page 64 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Static Aerodynamic Characteristics of a Three-stage Rocket Vehicle Having Various Fin Configurations at Low Subsonic Mach Numbers and Angles of Attack Up to 28 ̊ by : Clarence A. Brown
Download or read book Static Aerodynamic Characteristics of a Three-stage Rocket Vehicle Having Various Fin Configurations at Low Subsonic Mach Numbers and Angles of Attack Up to 28 ̊ written by Clarence A. Brown and published by . This book was released on 1963 with total page 40 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Aerodynamic Characteristics Over a Mach Number Range of 1.40 to 2.78 of a Rocket-propelled Airplane Configuration Having a Low 52.20 Delta Wing and an Unswept Horizontal Tail by : Alan B. Kehlet
Download or read book Aerodynamic Characteristics Over a Mach Number Range of 1.40 to 2.78 of a Rocket-propelled Airplane Configuration Having a Low 52.20 Delta Wing and an Unswept Horizontal Tail written by Alan B. Kehlet and published by . This book was released on 1961 with total page 30 pages. Available in PDF, EPUB and Kindle. Book excerpt:
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 Static Stability and Separation Characteristics of a Two-stage Rocket Configuration at Mach Numbers from 1.57 to 4.50 by : Kenneth L. Turner
Download or read book Static Stability and Separation Characteristics of a Two-stage Rocket Configuration at Mach Numbers from 1.57 to 4.50 written by Kenneth L. Turner and published by . This book was released on 1960 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Journal of the Royal Aeronautical Society by :
Download or read book Journal of the Royal Aeronautical Society written by and published by . This book was released on 1962 with total page 914 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Aerodynamic Characteristics of a Model of an Inflatable-Sphere Launching Vehicle Under Simulated Conditions of Mach Number and Altitude by : Ross B. Robinson
Download or read book Aerodynamic Characteristics of a Model of an Inflatable-Sphere Launching Vehicle Under Simulated Conditions of Mach Number and Altitude written by Ross B. Robinson and published by . This book was released on 1960 with total page 12 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Aerodynamic Characteristics at a Mach Number of 3.10 of Several Fourth-stage Shapes of the Scout Research Vehicle by : Byron M. Jaquet
Download or read book Aerodynamic Characteristics at a Mach Number of 3.10 of Several Fourth-stage Shapes of the Scout Research Vehicle written by Byron M. Jaquet and published by . This book was released on 1961 with total page 22 pages. Available in PDF, EPUB and Kindle. Book excerpt:
