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Stability And Control Characteristics Of A 00667 Scale Model Of The Final Version Of The North American X 15 Research Airplane Configuration 3 At Transonic Speeds
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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:
Book Synopsis Aerodynamic Characteristics of a 0.0667-scale Model of the North American X-15 Research Airplane at Transonic Speeds by : Robert S. Osborne
Download or read book Aerodynamic Characteristics of a 0.0667-scale Model of the North American X-15 Research Airplane at Transonic Speeds written by Robert S. Osborne and published by . This book was released on 1959 with total page 116 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 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 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 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 Longitudinal Stability Characteristics at Transonic Speeds of a Rocket-propelled Model of an Airplane Having a 45 Degree Swept Wing of Aspect Ratio 6.0 by : John C. McFall
Download or read book Longitudinal Stability Characteristics at Transonic Speeds of a Rocket-propelled Model of an Airplane Having a 45 Degree Swept Wing of Aspect Ratio 6.0 written by John C. McFall and published by . This book was released on 1954 with total page 44 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 Low-speed Measurements of Oscillatory Lateral Stability Derivatives of a 1/7-scale Model of the North American X-15 Airplane by : John W. Paulson
Download or read book Low-speed Measurements of Oscillatory Lateral Stability Derivatives of a 1/7-scale Model of the North American X-15 Airplane written by John W. Paulson and published by . This book was released on 1959 with total page 32 pages. Available in PDF, EPUB and Kindle. Book excerpt:
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:
Book Synopsis Determination of Longitudinal Stability and Control Characteristics from Free-flight Model Tests with Results at Transonic Speeds for Three Airplane Configurations by : Clarence L. Gillis
Download or read book Determination of Longitudinal Stability and Control Characteristics from Free-flight Model Tests with Results at Transonic Speeds for Three Airplane Configurations written by Clarence L. Gillis and published by . This book was released on 1957 with total page 28 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 Subsonic Stability and Control Derivatives for an Unpowered, Remotely Piloted 3/8 Scale F-15 Airplane Model Obtained from Flight Test by : Kenneth W. Iliff
Download or read book Subsonic Stability and Control Derivatives for an Unpowered, Remotely Piloted 3/8 Scale F-15 Airplane Model Obtained from Flight Test written by Kenneth W. Iliff and published by . This book was released on 1976 with total page 40 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis The Control Characteristics of Two 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 Control Characteristics of Two 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 1960 with total page 64 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Longitudinal Stability and Control Characteristics at High Subsonic Speeds of Two Models of a Transonic Research Airplane with Wings and Horizontal Tails of Aspect Ratios 4.2 and 2 by : Arvo A. Luoma
Download or read book Longitudinal Stability and Control Characteristics at High Subsonic Speeds of Two Models of a Transonic Research Airplane with Wings and Horizontal Tails of Aspect Ratios 4.2 and 2 written by Arvo A. Luoma and published by . This book was released on 1950 with total page 134 pages. Available in PDF, EPUB and Kindle. Book excerpt: An investigation was made in the Langley 8-foot high-speed tunnel of two transonic research airplane models for Mach numbers up to approximately 0.95. The test Reynolds number at the highest speed was 1,600,000 for one model and 2,300,000 for the other model. The models were 1/16-schale and were supported in the tunnel on a sting. The wing and horizontal tail of one model were both of aspect ratio 4.2; the wing and horizontal tail of the other model were both of aspect ratio 2. The same fuselage and vertical tail were used on both models. The sweep of the 50-percent-chord line of the wings was zero degrees; the sweep of the 75-percent-chord line of the horizontal tails was zero degrees. Both wings had NACA 65-110 airfoil sections and both horizontal tails had NACA 65-008 airfoil sections. Lift drag, and pitching moment were determined by means of a strain-gage balance within the fuselage. Tare measurements were made to eliminate the interference effect of the sting.
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 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:
