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Effects Of External Stores On The Aerodynamic Characteristics Of A 60 Delta Wing Fighter Model At Mach 160 To 287
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Book Synopsis Effects of External Stores on the Aerodynamic Characteristics of a 60 Deg Delta-wing Fighter Model at Mach 1.60 to 2.87 by :
Download or read book Effects of External Stores on the Aerodynamic Characteristics of a 60 Deg Delta-wing Fighter Model at Mach 1.60 to 2.87 written by and published by . This book was released on 1977 with total page 40 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Effects of External Stores on the Aerodynamic Characteristics of a 60 D̊elta-wing Fighter Model at Mach 1.60 to 2.87 by : M. Leroy Spearman
Download or read book Effects of External Stores on the Aerodynamic Characteristics of a 60 D̊elta-wing Fighter Model at Mach 1.60 to 2.87 written by M. Leroy Spearman and published by . This book was released on 1977 with total page 31 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis The Effect of Large External Stores on the Low-speed Longitudinal Aerodynamic Characteristics of a 60 ̊swept Delta Wing by : Lee Treadwell Allen
Download or read book The Effect of Large External Stores on the Low-speed Longitudinal Aerodynamic Characteristics of a 60 ̊swept Delta Wing written by Lee Treadwell Allen and published by . This book was released on 1955 with total page 82 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Effects of Size of External Stores on the Aerodynamic Characteristics of an Unswept and a 45 Degree Sweptback Wing of Aspect Ratio 4 and a 60 Degree Delta Wing at Mach Numbers of 1.41, 1.62, and 1.96 by : Carl R. Jacobsen
Download or read book Effects of Size of External Stores on the Aerodynamic Characteristics of an Unswept and a 45 Degree Sweptback Wing of Aspect Ratio 4 and a 60 Degree Delta Wing at Mach Numbers of 1.41, 1.62, and 1.96 written by Carl R. Jacobsen and published by . This book was released on 1953 with total page 55 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Effects of External Stores on the Static Longitudinal and Lateral Aerodynamic Characteristics of a Model of a 45 Degree Swept-wing Fighter Airplane at Mach Numbers of 1.61 and 2.01 by : Gerald V. Foster
Download or read book Effects of External Stores on the Static Longitudinal and Lateral Aerodynamic Characteristics of a Model of a 45 Degree Swept-wing Fighter Airplane at Mach Numbers of 1.61 and 2.01 written by Gerald V. Foster and published by . This book was released on 1956 with total page 38 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis The Effect of Large External Stores on the Low Speed Longitudinal Aerodynamic Characteristics of a 60 ̊delta Wing-fuselage Combination by : Wesley Merle Mann
Download or read book The Effect of Large External Stores on the Low Speed Longitudinal Aerodynamic Characteristics of a 60 ̊delta Wing-fuselage Combination written by Wesley Merle Mann and published by . This book was released on 1956 with total page 84 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Effects of External Stores on the Static Longitudinal Aerodynamic Characteristics of a Model of a 45 Degree Swept-wing Fighter Airplane at Mach Numbers of 1.61 and 2.01 by : Gerald V. Foster
Download or read book Effects of External Stores on the Static Longitudinal Aerodynamic Characteristics of a Model of a 45 Degree Swept-wing Fighter Airplane at Mach Numbers of 1.61 and 2.01 written by Gerald V. Foster and published by . This book was released on 1956 with total page 38 pages. Available in PDF, EPUB and Kindle. Book excerpt: An investigation has been conducted in the Langley 4- by 4-foot supersonic pressure tunnel to determine the effects of various external-store configurations of the longitudinal and lateral aerodynamic characteristics of a model of a 45 degree swept-wing fighter airplane. Pylon-mounted stores located at 23.8, 46.2, and 67.0 percent of the wing semispan were tested individually and in various combinations. The inboard stores relative to outboard stores were similar in shape but approximately 25 percent greater in size. The stores located at 46.2 percent of the wing semispan represented a large fuel tank and had an unsymmetrical shape.
Book Synopsis External Store Effects on the Stability of Fighter and Interceptor Airplanes by :
Download or read book External Store Effects on the Stability of Fighter and Interceptor Airplanes written by and published by . This book was released on 1974 with total page 34 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis The Aerodynamic Characteristics of Several Thick Delta Wings at Mach Numbers to 6 and Angles of Attack 50° by : John B. McDevitt
Download or read book The Aerodynamic Characteristics of Several Thick Delta Wings at Mach Numbers to 6 and Angles of Attack 50° written by John B. McDevitt and published by . This book was released on 1960 with total page 114 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis The Aerodynamic Characteristics of Several Thick Delta Wings at Mach Numbers to 6 and Angles of Attack 50 Deg by :
Download or read book The Aerodynamic Characteristics of Several Thick Delta Wings at Mach Numbers to 6 and Angles of Attack 50 Deg written by and published by . This book was released on 1966 with total page 108 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Aerodynamic Characteristics for Several Tip Controls on a 60° Delta Wing at Mach Number 1.61 by : Douglas R. Lord
Download or read book Aerodynamic Characteristics for Several Tip Controls on a 60° Delta Wing at Mach Number 1.61 written by Douglas R. Lord and published by . This book was released on 1954 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis A Note on the Drag Due to Lift of Delta Wings at Mach Numbers Up to 2.0 by : Robert S. Osborne
Download or read book A Note on the Drag Due to Lift of Delta Wings at Mach Numbers Up to 2.0 written by Robert S. Osborne and published by . This book was released on 1953 with total page 20 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Aerodynamic Characteristics of a Delta Wing with Leading Edge Swept Back 45 Degrees, Aspect Ratio 4, and NACA 65A006 Airfoil Section by : William C. Sleeman
Download or read book Aerodynamic Characteristics of a Delta Wing with Leading Edge Swept Back 45 Degrees, Aspect Ratio 4, and NACA 65A006 Airfoil Section written by William C. Sleeman and published by . This book was released on 1949 with total page 34 pages. Available in PDF, EPUB and Kindle. Book excerpt: This paper presents the results of the investigation of wing-alone and wing-fuselage combination employing a delta wing having 45 degree sweepback of the leading edge, aspect ratio 4, and an NACA 65A006 airfoil section. Lift, drag, pitching moment, and root bending moment were obtained for these configurations. In addition, effective downwash angles and dynamic-pressure characteristics in the region of a probable tail location also were obtained for these configurations, and are presented for a range of tail heights at one tail length. In order to expedite publishing of these data, only a brief analysis is included.
Book Synopsis Flow-field Characteristics and Aerodynamic Loads on External Stores Near the Fuselage and Wing-pylon Positions of a Swept-wing/fuselage Model at Mach Numbers of 0.4 and 0.7 by : R. H. Roberts
Download or read book Flow-field Characteristics and Aerodynamic Loads on External Stores Near the Fuselage and Wing-pylon Positions of a Swept-wing/fuselage Model at Mach Numbers of 0.4 and 0.7 written by R. H. Roberts and published by . This book was released on 1974 with total page 150 pages. Available in PDF, EPUB and Kindle. Book excerpt: Experimental data were obtained to aid in the prediction of aerodynamic loads and separation-trajectory characteristics on stores under the influence of an aircraft flow field. Four types of data were obtained in the vicinity of a generalized aircraft model: (1) flow field surveys, using a 40-deg cone probe, to determine the local velocity field, (2) force and moment data on four store models, (3) pressure distribution data on an ogive-cylinder model, and (4) captive-trajectory store separation data on one store model. The generalized aircraft model consisted of a swept-wing/fuselage combination with rectangular, flow-through engine ducts.
Book Synopsis The Effects of Wing-tip Droop on the Aerodynamic Characteristics of a Delta-wing Aircraft at Supersonic Speeds by :
Download or read book The Effects of Wing-tip Droop on the Aerodynamic Characteristics of a Delta-wing Aircraft at Supersonic Speeds written by and published by . This book was released on 1960 with total page 48 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Static Longitudinal and Lateral Aerodynamic Characteristics at a Mach Number of 2.20 of a Model of an 82 Deg Delta Wing Airplane Having Auxiliary Variable-sweep Wing Panels by :
Download or read book Static Longitudinal and Lateral Aerodynamic Characteristics at a Mach Number of 2.20 of a Model of an 82 Deg Delta Wing Airplane Having Auxiliary 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:
