Read Books Online and Download eBooks, EPub, PDF, Mobi, Kindle, Text Full Free.
Control Effectiveness And Tip Fin Dihedral Effects For The Hl 20 Lifting Body Configuration At Mach Numbers From 16 To 45
Download Control Effectiveness And Tip Fin Dihedral Effects For The Hl 20 Lifting Body Configuration At Mach Numbers From 16 To 45 full books in PDF, epub, and Kindle. Read online Control Effectiveness And Tip Fin Dihedral Effects For The Hl 20 Lifting Body Configuration At Mach Numbers From 16 To 45 ebook anywhere anytime directly on your device. Fast Download speed and no annoying ads. We cannot guarantee that every ebooks is available!
Book Synopsis Control Effectiveness and Tip-fin Dihedral Effects for the HL-20 Lifting-body Configuration at Mach Numbers from 1.6 to 4.5 by : Christopher I. Cruz
Download or read book Control Effectiveness and Tip-fin Dihedral Effects for the HL-20 Lifting-body Configuration at Mach Numbers from 1.6 to 4.5 written by Christopher I. Cruz and published by . This book was released on 1995 with total page 96 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author :National Aeronautics and Space Administration (NASA) Publisher :Createspace Independent Publishing Platform ISBN 13 :9781722322021 Total Pages :92 pages Book Rating :4.3/5 (22 download)
Book Synopsis Control Effectiveness and Tip-Fin Dihedral Effects for the Hl-20 Lifting-Body Configuration at Mach Numbers from 1.6 to 4.5 by : National Aeronautics and Space Administration (NASA)
Download or read book Control Effectiveness and Tip-Fin Dihedral Effects for the Hl-20 Lifting-Body Configuration at Mach Numbers from 1.6 to 4.5 written by National Aeronautics and Space Administration (NASA) and published by Createspace Independent Publishing Platform. This book was released on 2018-07-10 with total page 92 pages. Available in PDF, EPUB and Kindle. Book excerpt: Wind tunnel tests were made with a scale model of the HL-20 in the Langley Unitary Plan Wind Tunnel. Pitch control was investigated by deflecting the elevon surfaces on the outboard fins and body flaps on the fuselage. Yaw control tests were made with the all movable center fin deflected 5 deg. Almost full negative body flap deflection (-30 deg) was required to trim the HL-20 (moment reference center at 0.54-percent body length from nose) to positive values of life in the Mach number range from 1.6 to 2.5. Elevons were twice as effective as body flaps as a longitudinal trim device. The elevons were effective as a roll control, but because of tip-fin dihedral angle, produced about as much adverse yawing moment as rolling moment. The body flaps were less effective in producing rolling moment, but produced little adverse yawing moment. The yaw effectiveness of the all movable center fin was essentially constant over the angle-of-attack range at each Mach number. The value of yawing moment, however, was small. Center-fin deflection produced almost no rolling moments. The model was directionally unstable over most of the Mach number range with tip-fin dihedral angles less than the baseline value of 50 deg. Cruz, Christopher I. and Ware, George M. Langley Research Center...
Author :National Aeronautics and Space Administration (NASA) Publisher :Createspace Independent Publishing Platform ISBN 13 :9781720372783 Total Pages :60 pages Book Rating :4.3/5 (727 download)
Book Synopsis Aerodynamic Characteristics and Control Effectiveness of the Hl-20 Lifting Body Configuration at Mach 10 in Air by : National Aeronautics and Space Administration (NASA)
Download or read book Aerodynamic Characteristics and Control Effectiveness of the Hl-20 Lifting Body Configuration at Mach 10 in Air written by National Aeronautics and Space Administration (NASA) and published by Createspace Independent Publishing Platform. This book was released on 2018-05-29 with total page 60 pages. Available in PDF, EPUB and Kindle. Book excerpt: A 0.0196-scale model of the HL-20 lifting-body, one of several configurations proposed for future crewed spacecraft, was tested in the Langley 31-Inch Mach 10 Tunnel. The purpose of the tests was to determine the effectiveness of fin-mounted elevons, a lower surface flush-mounted body flap, and a flush-mounted yaw controller at hypersonic speeds. The nominal angle-of-attack range, representative of hypersonic entry, was 2 deg to 41 deg, the sideslip angles were 0 deg, 2 deg, and -2 deg, and the test Reynolds number was 1.06 x 10 E6 based on model reference length. The aerodynamic, longitudinal, and lateral control effectiveness along with surface oil flow visualizations are presented and discussed. The configuration was longitudinally and laterally stable at the nominal center of gravity. The primary longitudinal control, the fin-mounted elevons, could not trim the model to the desired entry angle of attack of 30 deg. The lower surface body flaps were effective for roll control and the associated adverse yawing moment was eliminated by skewing the body flap hinge lines. A yaw controller, flush-mounted on the lower surface, was also effective, and the associated small rolling moment was favorable.Scallion, William I.Langley Research CenterAERODYNAMIC CHARACTERISTICS; CONTROLLABILITY; EFFECTIVENESS; LIFTING BODIES; SCALE MODELS; WIND TUNNEL TESTS; ELEVONS; FINS; YAWING MOMENTS; STABILITY; SIDESLIP; REYNOLDS NUMBER; LONGITUDINAL CONTROL; LATERAL CONTROL; HYPERSONIC SPEED; FLOW VISUALIZATION; FLAPPING; ANGLE OF ATTACK
Book Synopsis Aerodynamic Chatacteristics and Control Effectiveness of the HL-20 Lifting Body Configuration at Mach 10 in Air by : William I. Scallion
Download or read book Aerodynamic Chatacteristics and Control Effectiveness of the HL-20 Lifting Body Configuration at Mach 10 in Air written by William I. Scallion and published by . This book was released on 1999 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Aerodynamic Characteristics and Control Effectiveness of the HL-20 Lifting Body Configuration at Mach 10 in Air by : William I. Scallion
Download or read book Aerodynamic Characteristics and Control Effectiveness of the HL-20 Lifting Body Configuration at Mach 10 in Air written by William I. Scallion and published by . This book was released on 1999 with total page 54 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Lift and Drag Characteristics of the HL-10 Lifting Body During Subsonic Gliding Flight by : Jon S. Pyle
Download or read book Lift and Drag Characteristics of the HL-10 Lifting Body During Subsonic Gliding Flight written by Jon S. Pyle and published by . This book was released on 1971 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Stability and Control Characteristics of a Flat-bottom Lifting Reentry Configuration at Mach Numbers of 2.29 to 4.63 by :
Download or read book Stability and Control Characteristics of a Flat-bottom Lifting Reentry Configuration at Mach Numbers of 2.29 to 4.63 written by and published by . This book was released on 1965 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Flight-determined Derivatives and Dynamic Characteristics for the HL-10 Lifting Body Vehicle at Subsonic and Transonic Mach Numbers by : Larry W. Strutz
Download or read book Flight-determined Derivatives and Dynamic Characteristics for the HL-10 Lifting Body Vehicle at Subsonic and Transonic Mach Numbers written by Larry W. Strutz and published by . This book was released on 1972 with total page 84 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis THE LONGITUDINAL AERODYNAMIC CHARACTERISTICS OF A RE-ENTRY CONFIGURATION BASED ON A BLUNT 13 DEG HALF-CONE AT MACH NUMBERS TO 0.92 by :
Download or read book THE LONGITUDINAL AERODYNAMIC CHARACTERISTICS OF A RE-ENTRY CONFIGURATION BASED ON A BLUNT 13 DEG HALF-CONE AT MACH NUMBERS TO 0.92 written by and published by . This book was released on 1961 with total page 68 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Effect of Elevon Deflection and of Model Components on Aerodynamic Characteristics of a Manned Lifting Entry Vehicle at Mach Numbers of 0.20 to 1.20 by :
Download or read book Effect of Elevon Deflection and of Model Components on Aerodynamic Characteristics of a Manned Lifting Entry Vehicle at Mach Numbers of 0.20 to 1.20 written by and published by . This book was released on 1966 with total page 84 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Full-scale Wind-tunnel Investigation of the Aerodynamic Characteristics of the HL-10 Manned Lifting Entry Vehicle by :
Download or read book Full-scale Wind-tunnel Investigation of the Aerodynamic Characteristics of the HL-10 Manned Lifting Entry Vehicle written by and published by . This book was released on 1965 with total page 52 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis The Lateral and Directional Aerodynamic Characteristics of a Re-entry Configuration Based on a Blunt 13 Deg Half Cone at Mach Numbers to 0.90 by :
Download or read book The Lateral and Directional Aerodynamic Characteristics of a Re-entry Configuration Based on a Blunt 13 Deg Half Cone at Mach Numbers to 0.90 written by and published by . This book was released on 1961 with total page 54 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Aerodynamic Interactions from Reaction Controls for Lateral Control of the M2-F2 Lifting-body Entry Configuration at Transonic and Supersonic and Supersonic Mach Numbers by :
Download or read book Aerodynamic Interactions from Reaction Controls for Lateral Control of the M2-F2 Lifting-body Entry Configuration at Transonic and Supersonic and Supersonic Mach Numbers written by and published by . This book was released on 1979 with total page 132 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis An Experimental Investigation of an Oblique-wing and Body Combination at Mach Numbers Between 0.60 and 1.40 by : Lawrence A. Graham
Download or read book An Experimental Investigation of an Oblique-wing and Body Combination at Mach Numbers Between 0.60 and 1.40 written by Lawrence A. Graham and published by . This book was released on 1972 with total page 378 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Effects of Body Shape on the Drag of a 45 Degree Sweptback-wing-body Configuration at Mach Numbers from 0.90 to 1.43 by : Walter B. Olstad
Download or read book Effects of Body Shape on the Drag of a 45 Degree Sweptback-wing-body Configuration at Mach Numbers from 0.90 to 1.43 written by Walter B. Olstad and published by . This book was released on 1958 with total page 66 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author :Jack Norman Nielsen Publisher :AIAA (American Institute of Aeronautics & Astronautics) ISBN 13 :9780962062902 Total Pages :450 pages Book Rating :4.0/5 (629 download)
Book Synopsis Missile Aerodynamics by : Jack Norman Nielsen
Download or read book Missile Aerodynamics written by Jack Norman Nielsen and published by AIAA (American Institute of Aeronautics & Astronautics). This book was released on 1988-01-01 with total page 450 pages. Available in PDF, EPUB and Kindle. Book excerpt: The similarities between the airplane and the missile extend beyond their flying capabilities, and at higher operational speeds, the configuration distinctions become even less apparent. " Missile Aerodynamics," a classic now available from AIAA and Nielsen Engineering and Research, Inc., combines the best of missile and airplane aerodynamics, drawing extensively from numerous technical papers to present a rational and unified account of the principles behind missile projection. Evaluate the missile versus the airplane in a multitude of areas, from longitudinal acceleration, wing loading, roll and dynamic stability, guidance and navigation, and more. J.N. Nielsen covers every aspect of missile aerodynamics, from the classification of missiles and basic formulas to innovative aerodynamic controls. In one reliable reference, readers will find hundreds of schematics, equations, and tables with practical applications in missile design and engineering. Originally published by Nielsen Engineering and Research, Inc.
Download or read book Wingless Flight written by R. Dale Reed and published by University Press of Kentucky. This book was released on 2014-07-15 with total page 256 pages. Available in PDF, EPUB and Kindle. Book excerpt: Most lifting bodies, or "flying bathtubs" as they were called, were so ugly only an engineer could love them, and yet, what an elegant way to keep wings from burning off in supersonic flight between earth and orbit. Working in their spare time (because they couldn't initially get official permission), Dale Reed and his team of engineers demonstrated the potential of the design that led to the Space Shuttle. Wingless Flight takes us behind the scenes with just the right blend of technical information and fascinating detail (the crash of M2-F2 found new life as the opening credit for TV's "The Six Million Dollar Man"). The flying bathtub, itself, is finding new life as the proposed escape-pod for the Space Station.
