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ISBN 13 :
Total Pages : 46 pages
Book Rating : 4.:/5 (254 download)
Download or read book Aerodynamic Characteristics of the 140A/B Space Shuttle Orbiter at Mach 10.3 written by and published by . This book was released on 1979 with total page 46 pages. Available in PDF, EPUB and Kindle. Book excerpt:
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ISBN 13 :
Total Pages : 102 pages
Book Rating : 4.:/5 (317 download)
Download or read book Space Shuttle Orbiter Trimmed Center-of-gravity Extension Study. Volume 9: Effects of Configuration Modifications on the Aerodynamic Characteristics of the 140 A/B Orbiter at Mach Numbers of 1.5, 2.0, and 2.5 written by and published by . This book was released on 1985 with total page 102 pages. Available in PDF, EPUB and Kindle. Book excerpt:
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ISBN 13 :
Total Pages : 140 pages
Book Rating : 4.:/5 (317 download)
Download or read book Space Shuttle Orbiter Trimmed Center of Gravity Extension Study. Volume 1: Effects of Configuration Modifications on the Aerodynamic Characteristics of the 140 A/B Orbiter at Mach 10.3 written by and published by . This book was released on 1975 with total page 140 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Peter T. Bernot
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ISBN 13 :
Total Pages : 52 pages
Book Rating : 4.F/5 ( download)
Download or read book Aerodynamic Characteristics of the 140A/B Space Shuttle Orbiter at Mach 10.3 written by Peter T. Bernot and published by . This book was released on 1979 with total page 52 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Lawrence E. Putnam
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ISBN 13 :
Total Pages : 30 pages
Book Rating : 4.:/5 (11 download)
Download or read book Aerodynamic Characteristics of an Ogee-wing Space Shuttle Orbiter Concept at a Mach Number of 2.01 written by Lawrence E. Putnam and published by . This book was released on 1972 with total page 30 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Ernald B. Graves
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ISBN 13 :
Total Pages : 40 pages
Book Rating : 4.:/5 (496 download)
Download or read book Aerodynamic Characteristics of a 60° Swept Delta-wing Space Shuttle Orbiter at Mach Numbers 2.50, 3.90 and 4.60 written by Ernald B. Graves and published by . This book was released on 1972 with total page 40 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : W. Pelham Phillips
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ISBN 13 :
Total Pages : 97 pages
Book Rating : 4.:/5 (913 download)
Download or read book Space shuttle orbiter trimmed center-of-gravity extension study written by W. Pelham Phillips and published by . This book was released on 1985 with total page 97 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Leland Howard Jorgenson
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ISBN 13 :
Total Pages : 44 pages
Book Rating : 4.:/5 (31 download)
Download or read book Effects of Reynolds Number and Body Corner Radius on Aerodynamic Characteristics of a Space Shuttle-type Vehicle at Subsonic Mach Numbers written by Leland Howard Jorgenson and published by . This book was released on 1972 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt: Static aerodynamic forces and moments were measured to study the effects of Reynolds number and body corner radius on the aerodynamic characteristics of a straight wing space shuttle orbiter at subsonic speeds. A 0.02-scale model was tested at Mach numbers from 0.3 to 0.9 and Reynolds numbers from about 600,000 to 3 million, based on body width. The body alone and the body with its wing and horizontal tail attached were tested at angles of attack from 35 to 75 degrees. The effects of rounding the body corners at the junctures connecting the bottom and sides were investigated for corner radii from 0 to 8.5 percent of the body width. At low subsonic Mach numbers (free stream Mach number approximately equal 0.3) the aerodynamic characteristics are affected significantly by changes in Reynolds number and body corner radius. With increase in Mach number to free stream Mach number = 0.9 the effect of Reynolds number seems to vanish, but a significant effect of body corner radius remains.
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ISBN 13 :
Total Pages : 46 pages
Book Rating : 4.:/5 (317 download)
Download or read book The Effects of Lateral Aerodynamic Uncertainties on the Handling Qualities of the Space Shuttle Orbiter at Mach Numbers of 1.5 and .6 written by and published by . This book was released on 1981 with total page 46 pages. Available in PDF, EPUB and Kindle. Book excerpt:
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ISBN 13 :
Total Pages : 50 pages
Book Rating : 4.:/5 (317 download)
Download or read book Supersonic Aerodynamic Characteristics of a Space Shutter Orbiter Model at Angles of Attack from 20 Deg to 90 Deg written by and published by . This book was released on 1987 with total page 50 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : UNITED STATES. NATIONAL AERONAUTICS AND SPACE ADMINISTRATION.
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ISBN 13 :
Total Pages : 100 pages
Book Rating : 4.:/5 (131 download)
Download or read book AERODYNAMIC CHARACTERISTICS OF A 60 DEGREE SWEPT DELTA-WING SPACE SHUTTLE ORBITER AT MACH NUMBERS OF 2.50, 3.90, AND 4.60 written by UNITED STATES. NATIONAL AERONAUTICS AND SPACE ADMINISTRATION. and published by . This book was released on 1966 with total page 100 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : John W. Paulson
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ISBN 13 :
Total Pages : 66 pages
Book Rating : 4.:/5 (31 download)
Download or read book Aerodynamic Characteristics of a Large Aircraft to Transport Space Shuttle Orbiter Or Other External Payloads written by John W. Paulson and published by . This book was released on 1975 with total page 66 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : James C. Ellison
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ISBN 13 :
Total Pages : 36 pages
Book Rating : 4.:/5 (317 download)
Download or read book Supersonic Longitudinal Aerodynamic Characteristics of Two Space Shuttle Orbiter Configurations written by James C. Ellison and published by . This book was released on 1977 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Brent R. Cobleigh
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ISBN 13 :
Total Pages : 40 pages
Book Rating : 4.:/5 (317 download)
Download or read book Development of the X-33 Aerodynamic Uncertainty Model written by Brent R. Cobleigh and published by . This book was released on 1998 with total page 40 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : James Charles Ellison
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ISBN 13 :
Total Pages : 44 pages
Book Rating : 4.F/5 ( download)
Download or read book Influence of Orbital-maneuvering-system Fairings and Rudder Flare on the Transonic Aerodynamic Characteristics of a Space Shuttle Orbiter written by James Charles Ellison and published by . This book was released on 1975 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : National Aeronautics and Space Adm Nasa
Publisher : Independently Published
ISBN 13 : 9781724073310
Total Pages : 30 pages
Book Rating : 4.0/5 (733 download)
Download or read book Inviscid Flow Computations of the Shuttle Orbiter for Mach 10 and 15 and Angle of Attack 40 to 60 Degrees written by National Aeronautics and Space Adm Nasa and published by Independently Published. This book was released on 2018-09-26 with total page 30 pages. Available in PDF, EPUB and Kindle. Book excerpt: This report documents the results of a computational study done to compute the inviscid longitudinal aerodynamic characteristics of the Space Shuttle Orbiter for Mach numbers 10 and 15 at angles of attack of 40, 50, 55, and 60 degrees. These computations were done to provide limited aerodynamic data in support of the Orbiter contingency abort task. The Orbiter had all the control surfaces in the undeflected position. The unstructured grid software FELISA was used for these computations with the equilibrium air option. Normal and axial force coefficients and pitching moment coefficients were computed. The hinge moment coefficients of the body flap and the inboard and outboard elevons were also computed. These results were compared with Orbiter Air Data Book (OADB) data and those computed using GASP. The comparison with the GASP results showed very good agreement in Cm and Ca at all the points. The computed axial force coefficients were smaller than those computed by GASP. There were noticeable differences between the present results and those in the OADB at angles of attack greater than 50 degrees. Prabhu, Ramadas K. and Sutton, Kenneth (Technical Monitor) Langley Research Center NASA/CR-2001-211267, NAS 1.26:211267
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Author : National Aeronautics and Space Administration (NASA)
Publisher : Createspace Independent Publishing Platform
ISBN 13 : 9781724991676
Total Pages : 34 pages
Book Rating : 4.9/5 (916 download)
Download or read book Supersonic Longitudinal Aerodynamic Characteristics of Two Space Shuttle Orbiter Configurations. [conducted in the Langley Unitary Plan Wind Tunnel] written by National Aeronautics and Space Administration (NASA) and published by Createspace Independent Publishing Platform. This book was released on 2018-08-09 with total page 34 pages. Available in PDF, EPUB and Kindle. Book excerpt: An investigation was conducted to determine the supersonic longitudinal aerodynamic characteristics of 0.015 scale models of the Rockwell International 089B and 139B space shuttle orbiter configurations and the 139B orbiter with a modifier forebody. The models each had a 45 deg swept delta wing that was blended into the body with an 81 deg swept fillet to form a double delta planform. The vertical tail had a split rudder deflected 27.5 deg on each side to form a speed brake. Tests were conducted at Mach numbers of 2.5, 3.9, and 4.6 at a Reynolds number, based on the body length of the 089B model, of 4,150,000. Angles of attack varied from -4 deg to 44 deg at 0 deg sideslip. Ellison, J. C. Langley Research Center NASA-TM-74074, L-11787 RTOP 506-26-30-04...
