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Static Longitudinal Directional And Lateral Stability And Control Data At A Mach Number Of 683 Of The Final Configuration Of The X 15 Research Airplane
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Book Synopsis Static Longitudinal, Directional, and Lateral Stability and Control Data at a Mach Number of 6.83 of the Final Configuration of the X-15 Research Airplane by : Jim A. Penland
Download or read book Static Longitudinal, Directional, and Lateral Stability and Control Data at a Mach Number of 6.83 of the Final Configuration of the X-15 Research Airplane written by Jim A. Penland and published by . This book was released on 1960 with total page 150 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Static Longitudinal, Directional, and Lateral Stability and Control Data at a Mach Number of 6.83 of the Final Configuration of the X- 15 Research Airplane by :
Download or read book Static Longitudinal, Directional, and Lateral Stability and Control Data at a Mach Number of 6.83 of the Final Configuration of the X- 15 Research Airplane written by and published by . This book was released on 1960 with total page 78 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Static Longitudinal, Directional, and Lateral Stability and Control Data from an Investigation at a Mach Number of 6.83 of Two Developmental X-15 Airplane Configuration by : David E. Fetterman
Download or read book Static Longitudinal, Directional, and Lateral Stability and Control Data from an Investigation at a Mach Number of 6.83 of Two Developmental X-15 Airplane Configuration written by David E. Fetterman and published by . This book was released on 1960 with total page 87 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Static Longitudinal, Directional, and Lateral Stability and Control Data from an Investigation at a Mach Number of 6.83 of Two Developmental X-15 Airplane Configurations by :
Download or read book Static Longitudinal, Directional, and Lateral Stability and Control Data from an Investigation at a Mach Number of 6.83 of Two Developmental X-15 Airplane Configurations written by and published by . This book was released on 1960 with total page 92 pages. Available in PDF, EPUB and Kindle. Book excerpt:
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:
Book Synopsis Static Longitudinal and Lateral Stability and Control Data from an Exploratory Investigation at a Mach Number of 6.86 of an Airplane Configuration Having a Wing of Trapezoidal Plan Form by : David E. Jr Fetterman
Download or read book Static Longitudinal and Lateral Stability and Control Data from an Exploratory Investigation at a Mach Number of 6.86 of an Airplane Configuration Having a Wing of Trapezoidal Plan Form written by David E. Jr Fetterman and published by . This book was released on 1955 with total page 103 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Stability and Control Derivative Characteristics of the X-15 Airplane by : Harold J. Walker
Download or read book Stability and Control Derivative Characteristics of the X-15 Airplane written by Harold J. Walker and published by . This book was released on 1962 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Static Lateral Characteristics at High Subsonic Speeds of a Complete Airplane Model with a Highly Tapered Wing Having the 0.80 Chord Line Unswept and with Several Tail Configuration by : Kenneth W. Goodson
Download or read book Static Lateral Characteristics at High Subsonic Speeds of a Complete Airplane Model with a Highly Tapered Wing Having the 0.80 Chord Line Unswept and with Several Tail Configuration written by Kenneth W. Goodson and published by . This book was released on 1961 with total page 102 pages. Available in PDF, EPUB and Kindle. Book excerpt: An investigation was made at high subsonic speeds of a complete model having a highly tapered wing and several tail configurations. The aspect-ratio-3.50 wing had a taper of 0.067 and an unswept 0.80 chord line. The complete model was tested with a wing-chord-plane tail, a T-tail, and a biplane tail (combined T-tail and wing-chord-plane tail). The model was tested in the Langley high-speed 7- by 10-foot tunnel at Mach numbers from 0.60 to 0.92 over a range of angle of attack of about ±20° and a range of sideslip of -15° to 13°. Some data were obtained with the horizontal stabilizer deflected. A few tests were also made with the wing tips clipped to an aspect ratio of 3.00.
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 1978 with total page 996 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 Static Longitudinal and Lateral Stability Characteristics at a Mach Number of 3.11 of Square and Circular Plan-form Reentry Vehicles, with Some Effects of Controls and Leading-edge Extensions by : Byron M. Jaquet
Download or read book Static Longitudinal and Lateral Stability Characteristics at a Mach Number of 3.11 of Square and Circular Plan-form Reentry Vehicles, with Some Effects of Controls and Leading-edge Extensions written by Byron M. Jaquet and published by . This book was released on 1960 with total page 26 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Static Longitudinal and Lateral Stability and Control Characteristics of a Model of a 35 Degree Swept-wing Airplane at a Mach Number of 1.41 by : Edward B. Palazzo
Download or read book Static Longitudinal and Lateral Stability and Control Characteristics of a Model of a 35 Degree Swept-wing Airplane at a Mach Number of 1.41 written by Edward B. Palazzo and published by . This book was released on 1955 with total page 30 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Static Stability and Control Characteristics of a Half-cone Entry Configuration at Mach Numbers from 2.2 to 0.7 by : Ralph W. Holtzclaw
Download or read book Static Stability and Control Characteristics of a Half-cone Entry Configuration at Mach Numbers from 2.2 to 0.7 written by Ralph W. Holtzclaw and published by . This book was released on 1962 with total page 68 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Some Data on the Static Longitudinal Stability and Control of Airplanes by : A. Martinov
Download or read book Some Data on the Static Longitudinal Stability and Control of Airplanes written by A. Martinov and published by . This book was released on 1940 with total page 672 pages. Available in PDF, EPUB and Kindle. Book excerpt: In the solution of a number of problems on the stability and controllability of airplanes, there arises the necessity for knowing the characteristics of the tail surfaces of the types in common use today. Of those characteristics, the most important are the effectiveness and hinge moments of the tail surfaces. As has been shown in the present paper, there exists the possibility of determining these characteristics by the formulas obtained with a degree of accuracy sufficient for the purposes of preliminary computation. These formulas take into account a number of fundamental tail characteristics such as tail cut-outs on the control surface and the form of the control surface leading edge.
Book Synopsis Static Longitudinal and Lateral Stability Data from an Exploratory Investigation at Mach Number 4.06 of an Airplane Configuration Having a Wing of Trapezoidal Plan Form by : Robert W. Dunning
Download or read book Static Longitudinal and Lateral Stability Data from an Exploratory Investigation at Mach Number 4.06 of an Airplane Configuration Having a Wing of Trapezoidal Plan Form written by Robert W. Dunning and published by . This book was released on 1955 with total page 37 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Flight Measurements of Stability and Control Derivatives of the X-15 Research Airplane to a Mach Number of 6.02 and an Angle of Attack of 250 by : Roxanah B. Yancey
Download or read book Flight Measurements of Stability and Control Derivatives of the X-15 Research Airplane to a Mach Number of 6.02 and an Angle of Attack of 250 written by Roxanah B. Yancey and published by . This book was released on 1964 with total page 56 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis The Static Stability Characteristics of Several Preliminary Models of the X-15 Research Airplane at Mach Numbers of 2.98 and 4.01 by : Robert W. Dunning
Download or read book The Static Stability Characteristics of Several Preliminary Models of the X-15 Research Airplane at Mach Numbers of 2.98 and 4.01 written by Robert W. Dunning and published by . This book was released on 1959 with total page 66 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Analysis of a Pilot-airplane Lateral Instability Experienced with the X-15 Airplane by : Lawrence W. Taylor
Download or read book Analysis of a Pilot-airplane Lateral Instability Experienced with the X-15 Airplane written by Lawrence W. Taylor and published by . This book was released on 1961 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt:
