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The Effects Of Lateral Aerodynamic Uncertainties On The Handling Qualities Of The Space Shuttle Orbiter At Mach Numbers Of 15 And 6
Download The Effects Of Lateral Aerodynamic Uncertainties On The Handling Qualities Of The Space Shuttle Orbiter At Mach Numbers Of 15 And 6 full books in PDF, epub, and Kindle. Read online The Effects Of Lateral Aerodynamic Uncertainties On The Handling Qualities Of The Space Shuttle Orbiter At Mach Numbers Of 15 And 6 ebook anywhere anytime directly on your device. Fast Download speed and no annoying ads. We cannot guarantee that every ebooks is available!
Book Synopsis The Effects of Lateral Aerodynamic Uncertainties on the Handling Qualities of the Space Shuttle Orbiter at Mach Numbers of 1.5 and .6 by :
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:
Book Synopsis Effects of Reynolds Number and Body Corner Radius on Aerodynamic Characteristics of a Space Shuttle-type Vehicle at Subsonic Mach Numbers by : Leland Howard Jorgenson
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.
Book Synopsis Effect of Aerodynamic and Angle-of-attack Uncertainties on the Blended Entry Flight Control System of the Space Shuttle from Mach 10 to 2.5 by : Howard W. Stone
Download or read book Effect of Aerodynamic and Angle-of-attack Uncertainties on the Blended Entry Flight Control System of the Space Shuttle from Mach 10 to 2.5 written by Howard W. Stone and published by . This book was released on 1984 with total page 296 pages. Available in PDF, EPUB and Kindle. Book excerpt:
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 1995 with total page 702 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Development of the X-33 Aerodynamic Uncertainty Model by : Brent R. Cobleigh
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:
Book Synopsis Aerodynamic Characteristics of the 140A/B Space Shuttle Orbiter at Mach 10.3 by : Peter T. Bernot
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:
Book Synopsis Effect of Aerodynamic and Angle-of-attack Uncertainties on the May 1979 Entry Flight Control System of the Space Shuttle from Mach 8 to 1.5 by : Howard W. Stone
Download or read book Effect of Aerodynamic and Angle-of-attack Uncertainties on the May 1979 Entry Flight Control System of the Space Shuttle from Mach 8 to 1.5 written by Howard W. Stone and published by . This book was released on 1985 with total page 144 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Influence of Orbital-maneuvering-system Fairings and Rudder Flare on the Transonic Aerodynamic Characteristics of a Space Shuttle Orbiter by : James Charles Ellison
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:
Book Synopsis Effect of Aerodynamic and Angle-of-attack Uncertainties on the May 1979 Entry Flight Control System of the Space Shuttle from Mach 8 to 1.5 by :
Download or read book Effect of Aerodynamic and Angle-of-attack Uncertainties on the May 1979 Entry Flight Control System of the Space Shuttle from Mach 8 to 1.5 written by and published by . This book was released on 1985 with total page 144 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Effect of Reynolds Number on the Aerodynamic Stability and Control Characteristics of a 55 Deg Clipped-delta-wing Orbiter Configuration at Supersonic Mach Numbers by : A. B. Blair (Jr)
Download or read book Effect of Reynolds Number on the Aerodynamic Stability and Control Characteristics of a 55 Deg Clipped-delta-wing Orbiter Configuration at Supersonic Mach Numbers written by A. B. Blair (Jr) and published by . This book was released on 1976 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Aerodynamic and Flow-visualization Studies of Two Delta-wing Entry Vehicles at a Mach Number of 20.3 by : James P. Arrington
Download or read book Aerodynamic and Flow-visualization Studies of Two Delta-wing Entry Vehicles at a Mach Number of 20.3 written by James P. Arrington and published by . This book was released on 1973 with total page 80 pages. Available in PDF, EPUB and Kindle. Book excerpt: The longitudinal, lateral, and directional aerodynamic characteristics of two space shuttle concepts have been obtained in helium for operational flight Reynolds numbers at angles of attack from minus 10 to 55 deg. Included are elevon control deflections, roll control due to ailerons, and the effects of a nose modification. Selected results were compared with those derived from tangent-cone and Newtonian theories. Also included are results of a flow-visualization study consisting of electron-beam-illuminated flow and surface oil-flow patterns.
Author :National Aeronautics and Space Adm Nasa Publisher :Independently Published ISBN 13 :9781724073310 Total Pages :30 pages Book Rating :4.0/5 (733 download)
Book Synopsis Inviscid Flow Computations of the Shuttle Orbiter for Mach 10 and 15 and Angle of Attack 40 to 60 Degrees by : National Aeronautics and Space Adm Nasa
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
Book Synopsis NASA Scientific and Technical Publications by :
Download or read book NASA Scientific and Technical Publications written by and published by . This book was released on 1991 with total page 178 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book NASA Technical Paper written by and published by . This book was released on 1985 with total page 144 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Government Reports Annual Index by :
Download or read book Government Reports Annual Index written by and published by . This book was released on 1975 with total page 882 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Space Shuttle Technical Conference, Part 1 by :
Download or read book Space Shuttle Technical Conference, Part 1 written by and published by . This book was released on 1985 with total page 604 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author :National Aeronautics and Space Adm Nasa Publisher :Independently Published ISBN 13 :9781729047743 Total Pages :26 pages Book Rating :4.0/5 (477 download)
Book Synopsis Lateral and Longitudinal Stability and Control Parameters for the Space Shuttle Discovery as Determined from Flight Test Data by : National Aeronautics and Space Adm Nasa
Download or read book Lateral and Longitudinal Stability and Control Parameters for the Space Shuttle Discovery as Determined from Flight Test Data written by National Aeronautics and Space Adm Nasa and published by Independently Published. This book was released on 2018-10-22 with total page 26 pages. Available in PDF, EPUB and Kindle. Book excerpt: The Discovery vehicle was found to have longitudinal and lateral aerodynamic characteristics similar to those of the Columbia and Challenger vehicles. The values of the lateral and longitudinal parameters are compared with the preflight data book. The lateral parameters showed the same trends as the data book. With the exception of C sub l sub Beta for Mach numbers greater than 15, C sub n sub delta r for Mach numbers greater than 2 and for Mach numbers less than 1.5, where the variation boundaries were not well defined, ninety percent of the extracted values of the lateral parameters fell within the predicted variations. The longitudinal parameters showed more scatter, but scattered about the preflight predictions. With the exception of the Mach 1.5 to .5 region of the flight envelope, the preflight predictions seem a reasonable representation of the Shuttle aerodynamics. The models determined accounted for ninety percent of the actual flight time histories. Suit, William T. and Schiess, James R. Langley Research Center RTOP 506-46-21-01...
