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Longitudinal And Lateral Aerodynamic Characteristics At Mach Numbers From 060 To 463 For Two Variable Sweep Configurations
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Book Synopsis Longitudinal and Lateral Aerodynamic Characteristics at Mach Numbers from 0.60 to 4.63 for Two Variable-sweep Configurations by :
Download or read book Longitudinal and Lateral Aerodynamic Characteristics at Mach Numbers from 0.60 to 4.63 for Two Variable-sweep Configurations written by and published by . This book was released on 1965 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Longitudinal Aerodynamic Characteristics at Mach Numbers from 0.40 to 1.10 of a Blunted Right-trangular Pyramidal Lifting Reentry Configuration Employing Variable-sweep Wing Panels by : Bernard Spencer
Download or read book Longitudinal Aerodynamic Characteristics at Mach Numbers from 0.40 to 1.10 of a Blunted Right-trangular Pyramidal Lifting Reentry Configuration Employing Variable-sweep Wing Panels written by Bernard Spencer and published by . This book was released on 1963 with total page 80 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Longitudinal and Lateral Aerodynamic Characteristics at Mach Numbers from 0.60 to 2.20 of a Variable Sweep Fighter Model with Wing Sweep Angles from 25 Deg to 75 Deg by :
Download or read book Longitudinal and Lateral Aerodynamic Characteristics at Mach Numbers from 0.60 to 2.20 of a Variable Sweep Fighter Model with Wing Sweep Angles from 25 Deg to 75 Deg written by and published by . This book was released on 1962 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Longitudinal Aerodynamic Characteristics at Mach Numbers from 0.50 to 1.19 of a Supersonic Transport Model with a Modified M Wing by : Edward J. Ray
Download or read book Longitudinal Aerodynamic Characteristics at Mach Numbers from 0.50 to 1.19 of a Supersonic Transport Model with a Modified M Wing written by Edward J. Ray and published by . This book was released on 1967 with total page 84 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis The Longitudinal and Lateral Aerodynamic Characteristics at Mach Numbers from 0.60 to 1.20 of a Variable-sweep Fighter Model with Wing Sweeps Varying from 25 Deg to 75 Deg by :
Download or read book The Longitudinal and Lateral Aerodynamic Characteristics at Mach Numbers from 0.60 to 1.20 of a Variable-sweep Fighter Model with Wing Sweeps Varying from 25 Deg to 75 Deg written by and published by . This book was released on 1963 with total page 78 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Longitudinal and Lateral Aerodynamic Characteristics at Mach Numbers of 3.00, 3.96, and 4.65 of a Low-fineness-ratio Elliptical Hypersonic Configuration Having Variable-sweep Wing Panels by :
Download or read book Longitudinal and Lateral Aerodynamic Characteristics at Mach Numbers of 3.00, 3.96, and 4.65 of a Low-fineness-ratio Elliptical Hypersonic Configuration Having Variable-sweep Wing Panels written by and published by . This book was released on 1963 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis The Longitudinal and Lateral Aerodynamic Characteristics at Mach Numbers of 1.41 and 2.20 of a Variable-sweep Fighter Model with Wing Sweeps Varying from 25 Deg to 75 Deg by :
Download or read book The Longitudinal and Lateral Aerodynamic Characteristics at Mach Numbers of 1.41 and 2.20 of a Variable-sweep Fighter Model with Wing Sweeps Varying from 25 Deg to 75 Deg written by and published by . This book was released on 1963 with total page 84 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Static Longitudinal and Lateral Aerodynamic Characteristics at a Mach Number of 2.01 of a Tailless Delta V/STOL Configuration Having Variable-sweep Wing Panels by :
Download or read book Static Longitudinal and Lateral Aerodynamic Characteristics at a Mach Number of 2.01 of a Tailless Delta V/STOL Configuration Having Variable-sweep Wing Panels written by and published by . This book was released on 1961 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Longitudinal and Lateral Aerodynamic Characteristics at Mach Numbers of 1.61 and 2.20 of a Variable Sweep Tactical Fighter Model with Wing Sweeps of 65 Deg, 85 Deg, and 106 Deg by :
Download or read book Longitudinal and Lateral Aerodynamic Characteristics at Mach Numbers of 1.61 and 2.20 of a Variable Sweep Tactical Fighter Model with Wing Sweeps of 65 Deg, 85 Deg, and 106 Deg written by and published by . This book was released on 1962 with total page 64 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Aerodynamic Characteristics at Mach Numbers from 2.50 to 4.63 of a Variablesweep Model at Sweep Angles from 55 Deg to 75 Deg by :
Download or read book Aerodynamic Characteristics at Mach Numbers from 2.50 to 4.63 of a Variablesweep Model at Sweep Angles from 55 Deg to 75 Deg written by and published by . This book was released on 1964 with total page 46 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Longitudinal Aerodynamic Characteristics at Mach Numbers from 0.28 to 2.50 of a Multipurpose Tactical Airplane Configuration Having Variable-sweep Wings and Externally Mounted Engines by :
Download or read book Longitudinal Aerodynamic Characteristics at Mach Numbers from 0.28 to 2.50 of a Multipurpose Tactical Airplane Configuration Having Variable-sweep Wings and Externally Mounted Engines written by and published by . This book was released on 1963 with total page 116 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Static Longitudinal and Lateral Aerodynamic Characteristic at a Mach Number of 2.20 of a Variable Sweep Fighter Airplane Configuration Having Body Mounted Nacelles with Vertical Ramp Inlets by :
Download or read book Static Longitudinal and Lateral Aerodynamic Characteristic at a Mach Number of 2.20 of a Variable Sweep Fighter Airplane Configuration Having Body Mounted Nacelles with Vertical Ramp Inlets written by and published by . This book was released on 1963 with total page 68 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Aerodynamic Characteristics at a Mach Number of 2.20 of a Variable-sweep Fighter Model with Wing Sweep of 50 Deg, 60 Deg, and 75 Deg by :
Download or read book Aerodynamic Characteristics at a Mach Number of 2.20 of a Variable-sweep Fighter Model with Wing Sweep of 50 Deg, 60 Deg, and 75 Deg written by and published by . This book was released on 1964 with total page 38 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Longitudinal Aerodynamic Characteristics of Several High-drag Bodies at Mach Numbers from 1.50 to 4.63 by : James F. Campbell
Download or read book Longitudinal Aerodynamic Characteristics of Several High-drag Bodies at Mach Numbers from 1.50 to 4.63 written by James F. Campbell and published by . This book was released on 1967 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Longitudinal Aerodynamic Characteristics at Mach Numbers from 0.40 to 1.10 of a Blunted Right-trangular Pyramidal Lifting Reentry Configuration Employing Variable-sweep Wing Panels by : Bernard Spencer
Download or read book Longitudinal Aerodynamic Characteristics at Mach Numbers from 0.40 to 1.10 of a Blunted Right-trangular Pyramidal Lifting Reentry Configuration Employing Variable-sweep Wing Panels written by Bernard Spencer and published by . This book was released on 1963 with total page 69 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Aerodynamic Characteristics at Mach Numbers from 1.50 to 4.63 of a Variable-geometry Lifting Reentry Concept Employing Elevator and Body Base Flaps for Control by : Roger H. Fournier
Download or read book Aerodynamic Characteristics at Mach Numbers from 1.50 to 4.63 of a Variable-geometry Lifting Reentry Concept Employing Elevator and Body Base Flaps for Control written by Roger H. Fournier and published by . This book was released on 1967 with total page 76 pages. Available in PDF, EPUB and Kindle. Book excerpt: An investigation of a lifting body configuration has been conducted in the Langley Unitary Plan wind tunnel through a Mach number range from 1.50 to 4.63 to determine the control effectiveness characteristics of body base flaps with and without anhedral tail elevator controls.
Book Synopsis Effect of Reynolds Number on the Low-speed Longitudinal Aerodynamic Characteristics of Two Variable-wing-sweep Airplane Configurations by :
Download or read book Effect of Reynolds Number on the Low-speed Longitudinal Aerodynamic Characteristics of Two Variable-wing-sweep Airplane Configurations written by and published by . This book was released on 1961 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt: