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Effect Of Speed Brakes On The Supersonic Aerodynamic Characteristics Of A Variable Sweep Tactical Fighter Model At Mach Numbers From 160 To 250
Download Effect Of Speed Brakes On The Supersonic Aerodynamic Characteristics Of A Variable Sweep Tactical Fighter Model At Mach Numbers From 160 To 250 full books in PDF, epub, and Kindle. Read online Effect Of Speed Brakes On The Supersonic Aerodynamic Characteristics Of A Variable Sweep Tactical Fighter Model At Mach Numbers From 160 To 250 ebook anywhere anytime directly on your device. Fast Download speed and no annoying ads. We cannot guarantee that every ebooks is available!
Book Synopsis Effect of Speed Brakes on the Supersonic Aerodynamic Characteristics of a Variable-sweep Tactical Fighter Model at Mach Numbers from 1.60 to 2.50 by : Celia S. Richardson
Download or read book Effect of Speed Brakes on the Supersonic Aerodynamic Characteristics of a Variable-sweep Tactical Fighter Model at Mach Numbers from 1.60 to 2.50 written by Celia S. Richardson and published by . This book was released on 1968 with total page 40 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 Low-speed Investigation of the Aerodynamic Characteristics of a Variable-sweep Supersonic Transport Configuration Having a Blended Wing and Body by : William C. Sleeman
Download or read book Low-speed Investigation of the Aerodynamic Characteristics of a Variable-sweep Supersonic Transport Configuration Having a Blended Wing and Body written by William C. Sleeman and published by . This book was released on 1961 with total page 68 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 Low-speed Longitudinal Aerodynamic Characteristics of a Supersonic Transport Model Having a Variable-sweep M Wing by :
Download or read book Low-speed Longitudinal Aerodynamic Characteristics of a Supersonic Transport Model Having a Variable-sweep M Wing written by and published by . This book was released on 1965 with total page 76 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Low-speed Investigation of the Aerodynamic Characteristics of a Variable-sweep Supersonic Transport Configuration Having a Blended Wing and Body by :
Download or read book Low-speed Investigation of the Aerodynamic Characteristics of a Variable-sweep Supersonic Transport Configuration Having a Blended Wing and Body written by and published by . This book was released on 1961 with total page 68 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Aerodynamic Characteristics at Mach Numbers from 0.50 to 2.96 of a Supersonic Transport Model with a Variable-sweep High-panel-aspect-ratio Wing by :
Download or read book Aerodynamic Characteristics at Mach Numbers from 0.50 to 2.96 of a Supersonic Transport Model with a Variable-sweep High-panel-aspect-ratio Wing written by and published by . This book was released on 1964 with total page 94 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 Aerodynamic Characteristics at Mach Numbers from 2.30 to 4.63 of a Supersonic Transport Model with a Variable-sweep M Wing by :
Download or read book Aerodynamic Characteristics at Mach Numbers from 2.30 to 4.63 of a Supersonic Transport Model with a Variable-sweep M Wing written by and published by . This book was released on 1965 with total page 100 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Low-speed Aerodynamic Characteristics of a Supersonic Transport Model with a High-aspect-ratio Variable-sweep Warped Wing by :
Download or read book Low-speed Aerodynamic Characteristics of a Supersonic Transport Model with a High-aspect-ratio Variable-sweep Warped Wing written by and published by . This book was released on 1964 with total page 62 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Aerodynamic Characteristics of a Three-engine Supersonic Transport Model Having a Low-aspect-ratio Variable-sweep Warped Wing by : Odell A. Morris
Download or read book Aerodynamic Characteristics of a Three-engine Supersonic Transport Model Having a Low-aspect-ratio Variable-sweep Warped Wing written by Odell A. Morris and published by . This book was released on 1964 with total page 72 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Low-speed Characteristics of a Variable-sweep Supersonic Transport Model with a Blended Engine Fuselage and Engine-mounted Tails by :
Download or read book Low-speed Characteristics of a Variable-sweep Supersonic Transport Model with a Blended Engine Fuselage and Engine-mounted Tails written by and published by . This book was released on 1964 with total page 86 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Aerodynamic Characteristics of a Three-engine Supersonic Transport Model Having a Low- Aspect-ratio Variable-sweep Warped Wing by :
Download or read book Aerodynamic Characteristics of a Three-engine Supersonic Transport Model Having a Low- Aspect-ratio Variable-sweep Warped Wing written by and published by . This book was released on 1964 with total page 70 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Transonic Longitudinal Aerodynamic Characteristics of a Variable-sweep Fighter Model Having Body-mounted Nacelles by :
Download or read book Transonic Longitudinal Aerodynamic Characteristics of a Variable-sweep Fighter Model Having Body-mounted Nacelles written by and published by . This book was released on 1964 with total page 54 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Stability and Control Characteristics at a Mach Number of 1.41 of a Variable-sweep Airplane Configuration Capable of Low-level Supersonic Attack-outer Wing Swept 75 Deg and 108 Deg by :
Download or read book Stability and Control Characteristics at a Mach Number of 1.41 of a Variable-sweep Airplane Configuration Capable of Low-level Supersonic Attack-outer Wing Swept 75 Deg and 108 Deg written by and published by . This book was released on 1960 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Transonic Aerodynamic Characteristics of Supersonic Transport Model with a Fixed, Warped Wing Having 74 Deg Sweep by :
Download or read book Transonic Aerodynamic Characteristics of Supersonic Transport Model with a Fixed, Warped Wing Having 74 Deg Sweep written by and published by . This book was released on 1965 with total page 60 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Supersonic Aerodynamic Characteristics of a Low-Drag Aircraft Configuration Having an Arrow Wing of Aspect Ratio 1.86 and a Body of Fineness Ratio 20 by :
Download or read book Supersonic Aerodynamic Characteristics of a Low-Drag Aircraft Configuration Having an Arrow Wing of Aspect Ratio 1.86 and a Body of Fineness Ratio 20 written by and published by . This book was released on 1960 with total page 80 pages. Available in PDF, EPUB and Kindle. Book excerpt: A free-flight rocket-propelled-model investigation was conducted at Mach numbers of 1.2 to 1.9 to determine the longitudinal and lateral aero-dynamic characteristics of a low-drag aircraft configuration. The model consisted of an aspect-ratio -1.86 arrow wing with 67.5 deg. leading-edge sweep and NACA 65A004 airfoil section and a triangular vertical tail with 60 deg. sweep and NACA 65A003 section in combination with a body of fineness ratio 20. Aerodynamic data in pitch, yaw, and roll were obtained from transient motions induced by small pulse rockets firing at intervals in the pitch and yaw directions. From the results of this brief aerodynamic investigation, it is observed that very slender body shapes can provide increased volumetric capacity with little or no increase in zero-lift drag and that body fineness ratios of the order of 20 should be considered in the design of long-range supersonic aircraft. The zero-lift drag and the drag-due-to-lift parameter of the test configuration varied linearly with Mach number. The maximum lift-drag ratio was 7.0 at a Mach number of 1.25 and decreased slightly to a value of 6.6 at a Mach number of 1.81. The optimum lift coefficient, normal-force-curve slope, lateral-force-curve slope, static stability in pitch and yaw, time to damp to one-half amplitude in pitch and yaw, the sum of the rotary damping derivatives in pitch and also in yaw, and the static rolling derivatives all decreased with an increase in Mach number. Values of certain rolling derivatives were obtained by application of the least-squares method to the differential equation of rolling motion. A comparison of the experimental and calculated total rolling-moment-coefficient variation during transient oscillations of the model indicated good agreement when the damping-in-roll contribution was included with the static rolling-moment terms.
