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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 Effect of Speed Brakes on the Supersonic Aerodynamical 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 Aerodynamical 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 33 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 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 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 The Transonic Aerodynamic Characteristics of Two Variable-sweep Airplane Configurations Capable of Low-level Supersonic Attack by : Ralph P. Bielat
Download or read book The Transonic Aerodynamic Characteristics of Two Variable-sweep Airplane Configurations Capable of Low-level Supersonic Attack written by Ralph P. Bielat and published by . This book was released on 1960 with total page 56 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Some Transonic and Supersonic Dynamic Stability Characteristics of a Variable-sweep-wing Tactical Fighter Model by : Robert A. Kilgore
Download or read book Some Transonic and Supersonic Dynamic Stability Characteristics of a Variable-sweep-wing Tactical Fighter Model written by Robert A. Kilgore and published by . This book was released on 1971 with total page 52 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 Aerodynamic Characteristics at Mach Numbers from 1.60 to 4.63 of a Variable-sweep Fighter Model with Wing Sweep Angles of 44° and 71° by : Milton Lamb
Download or read book Aerodynamic Characteristics at Mach Numbers from 1.60 to 4.63 of a Variable-sweep Fighter Model with Wing Sweep Angles of 44° and 71° written by Milton Lamb and published by . This book was released on 1972 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Effects of Various Modifications on the Supersonic Stability Characteristics of a Variable-wing-sweep Configuration at a Mach Number of 2.01 by :
Download or read book Effects of Various Modifications on the Supersonic Stability Characteristics of a Variable-wing-sweep Configuration at a Mach Number of 2.01 written by and published by . This book was released on 1960 with total page 42 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 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 :
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 Effect of Conventional and Square Stores on the Longitudinal Aerodynamic Characteristics of a Fighter Aircraft Model at Supersonic Speeds by : William J. Monta
Download or read book Effect of Conventional and Square Stores on the Longitudinal Aerodynamic Characteristics of a Fighter Aircraft Model at Supersonic Speeds written by William J. Monta and published by . This book was released on 1980 with total page 64 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Aerodynamic Characteristics at Mach Numbers from 0.6 to 2.16 of Supersonic Cruise Fighter Configuration with a Design Mach Mumber of 1.8 by : Barrett L. Shrout
Download or read book Aerodynamic Characteristics at Mach Numbers from 0.6 to 2.16 of Supersonic Cruise Fighter Configuration with a Design Mach Mumber of 1.8 written by Barrett L. Shrout and published by . This book was released on 1977 with total page 84 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Effects of Stores on Longitudinal Aerodynamic Characteristics of a Fighter at Supersonic Speeds by : Samuel M. Dollyhigh
Download or read book Effects of Stores on Longitudinal Aerodynamic Characteristics of a Fighter at Supersonic Speeds written by Samuel M. Dollyhigh and published by . This book was released on 1978 with total page 52 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.
