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Investigation Of The Low Subsonic Stability And Control Characteristics Of A 034 Scale Free Flying Model Of A Modified Half Cone Reentry Vehicle
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Book Synopsis Investigation of the Low-subsonic Stability and Control Characteristics of a 0.34-scale Free-flying Model of a Modified Half-cone Reentry Vehicle by : James L. Hassell
Download or read book Investigation of the Low-subsonic Stability and Control Characteristics of a 0.34-scale Free-flying Model of a Modified Half-cone Reentry Vehicle written by James L. Hassell and published by . This book was released on 1962 with total page 52 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Investigation of the Low-subsonic Stability and Control Characteristics of a 1/3-scale Free-flying Model of a Lifting-body Reentry Configuration by : James L. Hassell
Download or read book Investigation of the Low-subsonic Stability and Control Characteristics of a 1/3-scale Free-flying Model of a Lifting-body Reentry Configuration written by James L. Hassell and published by . This book was released on 1960 with total page 48 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 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 40 pages. Available in PDF, EPUB and Kindle. Book excerpt:
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 1963 with total page 162 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 Investigation of the Subsonic Stability and Control Characteristics of a 1/7-scale Model of the North American X-15 Airplane with and Without Fuselage Forebody Strakes by : James L. Hassell
Download or read book Investigation of the Subsonic Stability and Control Characteristics of a 1/7-scale Model of the North American X-15 Airplane with and Without Fuselage Forebody Strakes written by James L. Hassell and published by . This book was released on 1960 with total page 52 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 1963 with total page 1074 pages. Available in PDF, EPUB and Kindle. Book excerpt: Lists citations with abstracts for aerospace related reports obtained from world wide sources and announces documents that have recently been entered into the NASA Scientific and Technical Information Database.
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 Investigation of Low-subsonic Flight Characteristics of a Model of a Hypersonic Boost-glide Configuration Having a 78 Degree Delta Wing /by by : John W. Paulson
Download or read book Investigation of Low-subsonic Flight Characteristics of a Model of a Hypersonic Boost-glide Configuration Having a 78 Degree Delta Wing /by written by John W. Paulson and published by . This book was released on 1961 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Investigation of the Low-speed Stability and Control Characteristics of a 1/7-scale Model of the North American X-15 Airplane by : Peter C. Boisseau
Download or read book Investigation of the Low-speed Stability and Control Characteristics of a 1/7-scale Model of the North American X-15 Airplane written by Peter C. Boisseau and published by . This book was released on 1957 with total page 33 pages. Available in PDF, EPUB and Kindle. Book excerpt: An investigation of the low-speed power-on stability and control characteristics of a 1/7-scale free-flying model of the North American X-15 airplane has been made in the Langley Free-Flight Tunnel Section. The model was flown over an angle of attack range from 8 to 30 degrees, and only relatively low-altitude conditions were simulated.
Book Synopsis Investigation of the Low Subsonic Stability and Control Characteristics of a Hypersonic Boost Glide Type Airplane with Wing, Fuselage, and Vertical Tail Modifications by : Robert E. Shanks
Download or read book Investigation of the Low Subsonic Stability and Control Characteristics of a Hypersonic Boost Glide Type Airplane with Wing, Fuselage, and Vertical Tail Modifications written by Robert E. Shanks and published by . This book was released on 1961 with total page 52 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Investigation of the Low Subsonic Stability and Control Characteristics of a Model of a Hypersonic Boost-glide Airplane Designed for High Lift-drag Ratios at Low Speeds by :
Download or read book Investigation of the Low Subsonic Stability and Control Characteristics of a Model of a Hypersonic Boost-glide Airplane Designed for High Lift-drag Ratios at Low Speeds written by and published by . This book was released on 1961 with total page 46 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author :United States. National Aeronautics and Space Administration Scientific and Technical Information Division Publisher : ISBN 13 : Total Pages :1440 pages Book Rating :4.F/5 ( download)
Book Synopsis NASA Scientific and Technical Reports by : United States. National Aeronautics and Space Administration Scientific and Technical Information Division
Download or read book NASA Scientific and Technical Reports written by United States. National Aeronautics and Space Administration Scientific and Technical Information Division and published by . This book was released on 1966 with total page 1440 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Investigation of the Subsonic Stability and Control Characteristics of a 1/7-Scale Model of the North American X-15 Airplane with and Without Fuselage Forebody Strakes by :
Download or read book Investigation of the Subsonic Stability and Control Characteristics of a 1/7-Scale Model of the North American X-15 Airplane with and Without Fuselage Forebody Strakes written by and published by . This book was released on 1960 with total page 50 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Investigation of the Low-subsonic Flight Characteristics of a Model of a Supersonic Airplane Configuration Having Tail Surfaces Outboard of the Wing Tips by : Peter C. Boisseau
Download or read book Investigation of the Low-subsonic Flight Characteristics of a Model of a Supersonic Airplane Configuration Having Tail Surfaces Outboard of the Wing Tips written by Peter C. Boisseau and published by . This book was released on 1961 with total page 54 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author :United States. National Aeronautics and Space Administration. Scientific and Technical Information Division Publisher : ISBN 13 : Total Pages :1680 pages Book Rating :4.E/5 ( download)
Book Synopsis A Selected Listing of NASA Scientific and Technical Reports for ... by : United States. National Aeronautics and Space Administration. Scientific and Technical Information Division
Download or read book A Selected Listing of NASA Scientific and Technical Reports for ... written by United States. National Aeronautics and Space Administration. Scientific and Technical Information Division and published by . This book was released on 1965 with total page 1680 pages. Available in PDF, EPUB and Kindle. Book excerpt: