Stability and Control Characteristics of a 0.0667-scale Model of the Final Version of the North American X-15 Research Airplane (configuration 3) at Transonic Speeds

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ISBN 13 :
Total Pages : 112 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis Stability and Control Characteristics of a 0.0667-scale Model of the Final Version of the North American X-15 Research Airplane (configuration 3) at Transonic Speeds by : Robert S. Osborne

Download or read book Stability and Control Characteristics of a 0.0667-scale Model of the Final Version of the North American X-15 Research Airplane (configuration 3) at Transonic Speeds written by Robert S. Osborne and published by . This book was released on 1963 with total page 112 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Analysis and Design of Flight Vehicle Structures

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ISBN 13 :
Total Pages : 1008 pages
Book Rating : 4.3/5 (91 download)

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Book Synopsis Analysis and Design of Flight Vehicle Structures by : Elmer Franklin Bruhn

Download or read book Analysis and Design of Flight Vehicle Structures written by Elmer Franklin Bruhn and published by . This book was released on 1973 with total page 1008 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Investigation at Transonic Speeds of the Hinge-moment Characteristics of a 1/8-scale Model of the X-1E Aileron

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ISBN 13 :
Total Pages : 26 pages
Book Rating : 4.3/5 (91 download)

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Book Synopsis Investigation at Transonic Speeds of the Hinge-moment Characteristics of a 1/8-scale Model of the X-1E Aileron by : William C. Moseley (Jr.)

Download or read book Investigation at Transonic Speeds of the Hinge-moment Characteristics of a 1/8-scale Model of the X-1E Aileron written by William C. Moseley (Jr.) and published by . This book was released on 1955 with total page 26 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Investigation of the Static Lateral Stability and Aileron Characteristics of a 0.067-scale Model of the Bell X-2 Airplane at Mach Number of 2.29, 2.78, 3.22, and 3.71

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ISBN 13 :
Total Pages : 54 pages
Book Rating : 4.3/5 (91 download)

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Book Synopsis Investigation of the Static Lateral Stability and Aileron Characteristics of a 0.067-scale Model of the Bell X-2 Airplane at Mach Number of 2.29, 2.78, 3.22, and 3.71 by : Roger H. Fournier

Download or read book Investigation of the Static Lateral Stability and Aileron Characteristics of a 0.067-scale Model of the Bell X-2 Airplane at Mach Number of 2.29, 2.78, 3.22, and 3.71 written by Roger H. Fournier and published by . This book was released on 1958 with total page 54 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Aerodynamic and Landing Measurements Obtained During the First Powered Flight of the North American X-15 Research Airplane

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ISBN 13 :
Total Pages : 44 pages
Book Rating : 4.:/5 (317 download)

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Book Synopsis Aerodynamic and Landing Measurements Obtained During the First Powered Flight of the North American X-15 Research Airplane by :

Download or read book Aerodynamic and Landing Measurements Obtained During the First Powered Flight of the North American X-15 Research Airplane written by and published by . This book was released on 1960 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Transonic Longitudinal Aerodynamic Effects of Sweeping Up the Rear of the Fuselage of a Rocket-propelled Airplane Model Having No Horizontal Tail

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ISBN 13 :
Total Pages : 36 pages
Book Rating : 4.3/5 (91 download)

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Book Synopsis Transonic Longitudinal Aerodynamic Effects of Sweeping Up the Rear of the Fuselage of a Rocket-propelled Airplane Model Having No Horizontal Tail by : James H. Parks

Download or read book Transonic Longitudinal Aerodynamic Effects of Sweeping Up the Rear of the Fuselage of a Rocket-propelled Airplane Model Having No Horizontal Tail written by James H. Parks and published by . This book was released on 1955 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Design and Physical Characteristics of the Transonic Aircraft Technology (Tact) Research Aircraft

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Publisher : Createspace Independent Publishing Platform
ISBN 13 : 9781724282040
Total Pages : 32 pages
Book Rating : 4.2/5 (82 download)

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Book Synopsis Design and Physical Characteristics of the Transonic Aircraft Technology (Tact) Research Aircraft by : National Aeronautics and Space Administration (NASA)

Download or read book Design and Physical Characteristics of the Transonic Aircraft Technology (Tact) Research Aircraft written by National Aeronautics and Space Administration (NASA) and published by Createspace Independent Publishing Platform. This book was released on 2018-07-26 with total page 32 pages. Available in PDF, EPUB and Kindle. Book excerpt: The Transonic Aircraft Technology (TACT) research program provided data necessary to verify aerodynamic concepts, such as the supercritical wing, and to gain the confidence required for the application of such technology to advanced high performance aircraft. An F-111A aircraft was employed as the flight test bed to provide full scale data. The data were correlated extensively with predictions based on data obtained from wind tunnel tests. An assessment of the improvement afforded at transonic speeds in drag divergence, maneuvering performance, and airplane handling qualities by the use of the supercritical wing was included in the program. Transonic flight and wind tunnel testing techniques were investigated, and specific research technologies evaluated were also summarized. Painter, W. D. and Caw, L. J. Armstrong Flight Research Center NASA-TM-56048, H-976

Aerodynamic-derivative Characteristics of the X-15 Research Airplane as Determined from Flight Tests for Mach Numbers from 0.6 to 3.4

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ISBN 13 :
Total Pages : 72 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis Aerodynamic-derivative Characteristics of the X-15 Research Airplane as Determined from Flight Tests for Mach Numbers from 0.6 to 3.4 by : Roxanah B. Yancey

Download or read book Aerodynamic-derivative Characteristics of the X-15 Research Airplane as Determined from Flight Tests for Mach Numbers from 0.6 to 3.4 written by Roxanah B. Yancey and published by . This book was released on 1962 with total page 72 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Transonic Flutter Investigation of Models of the X-15 Airplane Horizontal Tail

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ISBN 13 :
Total Pages : 40 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis Transonic Flutter Investigation of Models of the X-15 Airplane Horizontal Tail by : Lou S. Young

Download or read book Transonic Flutter Investigation of Models of the X-15 Airplane Horizontal Tail written by Lou S. Young and published by . This book was released on 1961 with total page 40 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Preliminary Results for a Free-flight Investigation at Transonic and Supersonic Speeds of Longitudinal Stability and Control Characteristics of an Airplane Configuration with a Thin Straight Wing of Aspect Ratio 3

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ISBN 13 :
Total Pages : 64 pages
Book Rating : 4.3/5 (91 download)

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Book Synopsis Preliminary Results for a Free-flight Investigation at Transonic and Supersonic Speeds of Longitudinal Stability and Control Characteristics of an Airplane Configuration with a Thin Straight Wing of Aspect Ratio 3 by : Clarence L. Gillis

Download or read book Preliminary Results for a Free-flight Investigation at Transonic and Supersonic Speeds of Longitudinal Stability and Control Characteristics of an Airplane Configuration with a Thin Straight Wing of Aspect Ratio 3 written by Clarence L. Gillis and published by . This book was released on 1950 with total page 64 pages. Available in PDF, EPUB and Kindle. Book excerpt:

An Investigation at Transonic Speeds of the Effects of Thickness Ratio and of Thickened Root Sections on the Aerodynamic Characteristics of Wings with 47© Sweepback, Aspect Ratio 3.5, and Taper Ratio 0.2 in the Slotted Test Section of the Langley 8-foot High-speed Tunnel

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ISBN 13 :
Total Pages : 44 pages
Book Rating : 4.3/5 (91 download)

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Book Synopsis An Investigation at Transonic Speeds of the Effects of Thickness Ratio and of Thickened Root Sections on the Aerodynamic Characteristics of Wings with 47© Sweepback, Aspect Ratio 3.5, and Taper Ratio 0.2 in the Slotted Test Section of the Langley 8-foot High-speed Tunnel by : Ralph P. Bielat

Download or read book An Investigation at Transonic Speeds of the Effects of Thickness Ratio and of Thickened Root Sections on the Aerodynamic Characteristics of Wings with 47© Sweepback, Aspect Ratio 3.5, and Taper Ratio 0.2 in the Slotted Test Section of the Langley 8-foot High-speed Tunnel written by Ralph P. Bielat and published by . This book was released on 1951 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt: Four wing-body combinations of the same plan form (47 degree sweep, 3.5 aspect ratio, and 0.2 taper ratio) were compared at transonic speeds in the Langley 8-foot high-speed tunnel. Three wings were 4, 6, and 9 percent thick; the fourth was 6 percent thick but, on the inner 0.4 span, tapered to 12-percent thickness at the roots.

Longitudinal Aerodynamic Characteristics at Transonic Speeds of a V/STOL Airplane Configuration with a Fixed Delta Wing Having Auxiliary Variable-sweep Outboard Panels

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ISBN 13 :
Total Pages : 88 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis Longitudinal Aerodynamic Characteristics at Transonic Speeds of a V/STOL Airplane Configuration with a Fixed Delta Wing Having Auxiliary Variable-sweep Outboard Panels by : Arvo A. Luoma

Download or read book Longitudinal Aerodynamic Characteristics at Transonic Speeds of a V/STOL Airplane Configuration with a Fixed Delta Wing Having Auxiliary Variable-sweep Outboard Panels written by Arvo A. Luoma and published by . This book was released on 1961 with total page 88 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Drag of a Supercritical Body of Revolution in Free Flight at Transonic Speeds and Comparison with Wind-tunnel Data

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ISBN 13 :
Total Pages : 44 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis Drag of a Supercritical Body of Revolution in Free Flight at Transonic Speeds and Comparison with Wind-tunnel Data by : J. W. Usry

Download or read book Drag of a Supercritical Body of Revolution in Free Flight at Transonic Speeds and Comparison with Wind-tunnel Data written by J. W. Usry and published by . This book was released on 1971 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Hypersonic Aerodynamic Characteristics of Two Delta-wing X-15 Airplane Configurations

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Publisher :
ISBN 13 :
Total Pages : 108 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis Hypersonic Aerodynamic Characteristics of Two Delta-wing X-15 Airplane Configurations by : Theodore J. Goldberg

Download or read book Hypersonic Aerodynamic Characteristics of Two Delta-wing X-15 Airplane Configurations written by Theodore J. Goldberg and published by . This book was released on 1969 with total page 108 pages. Available in PDF, EPUB and Kindle. Book excerpt: Hypersonic aerodynamic characteristics of delta wing x- 15 airplane configurations.

An Investigation at Transonic Speeds of the Effects of Thickness Ratio and of Thickened Root Sections on the Aerodynamic Characteristics of Wings with 47° Sweepback, Aspect Ratio 3.5, and Taper Ratio 0.2 in the Slotted Test Section of the Langley 8-foot High-speed Tunnel

Download An Investigation at Transonic Speeds of the Effects of Thickness Ratio and of Thickened Root Sections on the Aerodynamic Characteristics of Wings with 47° Sweepback, Aspect Ratio 3.5, and Taper Ratio 0.2 in the Slotted Test Section of the Langley 8-foot High-speed Tunnel PDF Online Free

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ISBN 13 :
Total Pages : 38 pages
Book Rating : 4.:/5 (7 download)

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Book Synopsis An Investigation at Transonic Speeds of the Effects of Thickness Ratio and of Thickened Root Sections on the Aerodynamic Characteristics of Wings with 47° Sweepback, Aspect Ratio 3.5, and Taper Ratio 0.2 in the Slotted Test Section of the Langley 8-foot High-speed Tunnel by : Ralph P. Bielat

Download or read book An Investigation at Transonic Speeds of the Effects of Thickness Ratio and of Thickened Root Sections on the Aerodynamic Characteristics of Wings with 47° Sweepback, Aspect Ratio 3.5, and Taper Ratio 0.2 in the Slotted Test Section of the Langley 8-foot High-speed Tunnel written by Ralph P. Bielat and published by . This book was released on 1958 with total page 38 pages. Available in PDF, EPUB and Kindle. Book excerpt:

The Effects of Wing Plan Form on the Static Longitudinal Aerodynamic Characteristics of a Flat-top Hypersonic Aircraft at Mach Numbers from 0.6 to 1.4

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ISBN 13 :
Total Pages : 36 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis The Effects of Wing Plan Form on the Static Longitudinal Aerodynamic Characteristics of a Flat-top Hypersonic Aircraft at Mach Numbers from 0.6 to 1.4 by : Stuart L. Treon

Download or read book The Effects of Wing Plan Form on the Static Longitudinal Aerodynamic Characteristics of a Flat-top Hypersonic Aircraft at Mach Numbers from 0.6 to 1.4 written by Stuart L. Treon and published by . This book was released on 1960 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Transonic Aerodynamic Characteristics of a Variable-sweep Airplane Configuration Having a 12-percent-thick Wing and an Inboard Pivot Location

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ISBN 13 :
Total Pages : 84 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis Transonic Aerodynamic Characteristics of a Variable-sweep Airplane Configuration Having a 12-percent-thick Wing and an Inboard Pivot Location by : Ralph P. Bielat

Download or read book Transonic Aerodynamic Characteristics of a Variable-sweep Airplane Configuration Having a 12-percent-thick Wing and an Inboard Pivot Location written by Ralph P. Bielat and published by . This book was released on 1960 with total page 84 pages. Available in PDF, EPUB and Kindle. Book excerpt: