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Investigation Of The Low Subsonic Flight Characteristics Of A Model Of A Reentry Vehicle With A Thick Flat 75 Degree Swept Delta Wing And A Half Cone Fuselage
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Book Synopsis Investigation of the Low-subsonic Flight Characteristics of a Model of a Reentry Vehicle with a Thick Flat 75 Degree Swept Delta Wing and a Half-cone Fuselage by : Peter C. Boisseau
Download or read book Investigation of the Low-subsonic Flight Characteristics of a Model of a Reentry Vehicle with a Thick Flat 75 Degree Swept Delta Wing and a Half-cone Fuselage written by Peter C. Boisseau and published by . This book was released on 1962 with total page 38 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Investigation of the Low-subsonic Flight Characteristics of a Model of a Reentry Vehicle with a Thick Flat 75 Degree Swept Delta Wing and a Half-cone Fuselage by : Peter C. Boisseau
Download or read book Investigation of the Low-subsonic Flight Characteristics of a Model of a Reentry Vehicle with a Thick Flat 75 Degree Swept Delta Wing and a Half-cone Fuselage written by Peter C. Boisseau and published by . This book was released on 1962 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Investigation of the Low-subsonic Flight Characteristics of a Model of a Reentry Vehicle with a Thick Flat 75 Degrees Swept Delta Wing and a Half-cone Fuselage by : PETER C. BOISSEAU
Download or read book Investigation of the Low-subsonic Flight Characteristics of a Model of a Reentry Vehicle with a Thick Flat 75 Degrees Swept Delta Wing and a Half-cone Fuselage written by PETER C. BOISSEAU and published by . This book was released on 1962 with total page 1 pages. Available in PDF, EPUB and Kindle. Book excerpt: An investigation of the low-subsonic flight characteristics of a model having a thick flat 75 degrees swept delta wing with a half-cone fuselage on the upper surface was made in the Langley full-scale tunnel over an angle-ofattack range from about 20 to 40 degrees. Static and dynamic force test data were also obtained. The longitudinal flight characteristics were generally satisfactory over the angle-of-attack range of the investigation. Because of low damping of the Dutch roll oscillation, the lateral stability and control characteristics were poor throughout the angle-of-attack range (20 to 30 degrees) where flights were possible without artificial damping. Artificial damping in roll greatly improved the lateral characteristics so that flights could be made up to an angle of attack of about 40 degrees. (Author).
Book Synopsis U.S. Government Research Reports by :
Download or read book U.S. Government Research Reports written by and published by . This book was released on 1962 with total page 162 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Investigation of the Low-subsonic Flight Characteristics of a Model of a Reentry Configuration Having a 75 Deg Delta Wing by :
Download or read book Investigation of the Low-subsonic Flight Characteristics of a Model of a Reentry Configuration Having a 75 Deg Delta Wing written by and published by . This book was released on 1962 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Applied Mechanics Reviews written by and published by . This book was released on 1962 with total page 1116 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis An Investigation at Subsonic Speeds of the Longitudinal Aerodynamic Characteristics at Angles of Attach from -4° to 100° of Delta-wing Reentry Configurations Having Vertically Displaced and Cambered Wing-tip Panels by : Bernard Spencer
Download or read book An Investigation at Subsonic Speeds of the Longitudinal Aerodynamic Characteristics at Angles of Attach from -4° to 100° of Delta-wing Reentry Configurations Having Vertically Displaced and Cambered Wing-tip Panels written by Bernard Spencer and published by . This book was released on 1961 with total page 40 pages. Available in PDF, EPUB and Kindle. Book excerpt: Subsonic aerodynamic characteristics of delta-wing reentry vehicle with vertically displaced and cambered wing-tip panels.
Book Synopsis Monthly Catalog of United States Government Publications by :
Download or read book Monthly Catalog of United States Government Publications written by and published by . This book was released on 1962 with total page 1990 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Bibliography of Scientific and Industrial Reports by :
Download or read book Bibliography of Scientific and Industrial Reports written by and published by . This book was released on 1962 with total page 1116 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Investigation of the Low-subsonic Stability and Control Characteristics of a Free-flying Model of a Thick 70° Delta Reentry Configuration by : John W. Paulson
Download or read book Investigation of the Low-subsonic Stability and Control Characteristics of a Free-flying Model of a Thick 70° Delta Reentry Configuration written by John W. Paulson and published by . This book was released on 1961 with total page 34 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis ARS Journal by : American Rocket Society
Download or read book ARS Journal written by American Rocket Society and published by . This book was released on 1962 with total page 1024 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Investigation of the Low-subsonic Stability and Control Characteristics of a Free-flying Model of a Thick 70 Degree Delta Reentry Configuration by : JOHN W. PAULSON
Download or read book Investigation of the Low-subsonic Stability and Control Characteristics of a Free-flying Model of a Thick 70 Degree Delta Reentry Configuration written by JOHN W. PAULSON and published by . This book was released on 1961 with total page 1 pages. Available in PDF, EPUB and Kindle. Book excerpt: The longitudinal stability and control characteristics were considered satisfactory when the model had positive static longitud nal stability. It wa possible to fly the model with a small amount of static instability, but the longitudinal characteristics were considered unsatisfactory in this condition. At angles of attack above the stall the model developed a large, constant-amplitude pitching oscillation. The lateral stability characteristics were considered to be only fair at angles of attack from about 20 deg to 35 deg because of a lightly damped Dutch roll oscillation. At higher angles of attack the oscillation was well damped and the lateral stability was generally satisfactory. The Dutch roll damping at the lower angles of attack was increased to satisfactory values by means of a simple rate-type roll damper. The lateral control characteristics were generally satisfactory throughout the angle-of-attack range, but there was some deterioration in aileron effectiveness in the high angle-ofattack range due mainly to a large increase in damping in roll. (Author).
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 1966-12 with total page 1288 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Investigation of the Low-subsonic Stability and Control Characteristics of a Free-flying Model of a Thick 70 Degree Delta Reentrry Configuration by : John W. Paulson
Download or read book Investigation of the Low-subsonic Stability and Control Characteristics of a Free-flying Model of a Thick 70 Degree Delta Reentrry Configuration written by John W. Paulson and published by . This book was released on 1961 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Low-subsonic-speed Static Longitudinal Stability and Control Characteristics of a Winged Reentry-vehicle Configuration Having Wingtip Panels that Fold Up for High-drag Reentry by : George M. Ware
Download or read book Low-subsonic-speed Static Longitudinal Stability and Control Characteristics of a Winged Reentry-vehicle Configuration Having Wingtip Panels that Fold Up for High-drag Reentry written by George M. Ware and published by . This book was released on 1960 with total page 20 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis High-subsonic-speed Investigation of the Static Longitudinal Aerodynamic Characteristics of Several Delta-wing Configurations for Angles of Attack from 0° to 90° by : Bernard Spencer
Download or read book High-subsonic-speed Investigation of the Static Longitudinal Aerodynamic Characteristics of Several Delta-wing Configurations for Angles of Attack from 0° to 90° written by Bernard Spencer and published by . This book was released on 1959 with total page 34 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis International Aerospace Abstracts by :
Download or read book International Aerospace Abstracts written by and published by . This book was released on 1962 with total page 540 pages. Available in PDF, EPUB and Kindle. Book excerpt:
