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Aerodynamic Load Measurements And Opening Characteristics Of Automatic Leading Edge Slats On A 45c Sweptback Wing At Transonic Speeds
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Book Synopsis Aerodynamic Load Measurements and Opening Characteristics of Automatic Leading-edge Slats on a 45 Degree Sweptback Wing at Transonic Speeds by : Donald D. Arabian
Download or read book Aerodynamic Load Measurements and Opening Characteristics of Automatic Leading-edge Slats on a 45 Degree Sweptback Wing at Transonic Speeds written by Donald D. Arabian and published by . This book was released on 1961 with total page 54 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Aerodynamic Load Measurements and Opening Characteristics of Automatic Leading-edge Slats on a 45° Sweptback Wing at Transonic Speeds by : Donald D. Arabian
Download or read book Aerodynamic Load Measurements and Opening Characteristics of Automatic Leading-edge Slats on a 45° Sweptback Wing at Transonic Speeds written by Donald D. Arabian and published by . This book was released on 1961 with total page 49 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Aerodynamic Load Measurements and Opening Characteristics of Automatic Leading-edge Slats on a 45 Degree Sweptback Wing at Transonic Speeds by : Donald D. Arabian
Download or read book Aerodynamic Load Measurements and Opening Characteristics of Automatic Leading-edge Slats on a 45 Degree Sweptback Wing at Transonic Speeds written by Donald D. Arabian and published by . This book was released on 1954 with total page 49 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Aerodynamic Characteristics of a Leading-edge Slat on a 35 Degree Swept-back Wing for Mach Numbers from 0.30 to 0.88 by : John A. Kelly
Download or read book Aerodynamic Characteristics of a Leading-edge Slat on a 35 Degree Swept-back Wing for Mach Numbers from 0.30 to 0.88 written by John A. Kelly and published by . This book was released on 1951 with total page 56 pages. Available in PDF, EPUB and Kindle. Book excerpt: The data presented in this report were obtained by North American Aviation, Inc., from an investigation conducted in the Southern California Cooperative Wind Tunnel. Tests were made over a range of Mach numbers from 0.300 to 0.883 to determine the aerodynamic characteristics of a semispan model of a 35 degree swept-back wing equipped with a leading-edge slat and to gain additional knowledge of the aerodynamic loads and automatic operation of the slat. Lift, drag, and pitching-moment characteristics of a model wing in the presence of a fuselage were measured as well as pressures acting on the slat in the retracted and the full-open positions. The pressure data were analyzed to ascertain the opening characteristics of the slat for two possible circular-arc slat tracks which could be used for automatic operation of the slat.
Book Synopsis The Aerodynamic Characteristics at Transonic Speeds of a Model with a 45 Degree Sweptback Wing, Including Effect of Leading-edge Slats and a Low Horizontal Tail by : Jack F. Runckel
Download or read book The Aerodynamic Characteristics at Transonic Speeds of a Model with a 45 Degree Sweptback Wing, Including Effect of Leading-edge Slats and a Low Horizontal Tail written by Jack F. Runckel and published by . This book was released on 1954 with total page 60 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Aerodynamic Load Measurements Over a Leading-edge Slat on a 40 Degree Sweptback Wing at Mach Numbers from 0.10 to 0.91 by : Jones F. Cahill
Download or read book Aerodynamic Load Measurements Over a Leading-edge Slat on a 40 Degree Sweptback Wing at Mach Numbers from 0.10 to 0.91 written by Jones F. Cahill and published by . This book was released on 1952 with total page 32 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Investigation at Transonic Speeds of the Loading Over a 45 Degree Sweptback Wing Having an Aspect Ratio of 3, a Taper Ratio of 0.2, and NACA 65A004 Airfoil Sections by : Jack F. Runckel
Download or read book Investigation at Transonic Speeds of the Loading Over a 45 Degree Sweptback Wing Having an Aspect Ratio of 3, a Taper Ratio of 0.2, and NACA 65A004 Airfoil Sections written by Jack F. Runckel and published by . This book was released on 1956 with total page 104 pages. Available in PDF, EPUB and Kindle. Book excerpt: An investigation at transonic speeds of the loading over a 45 degree sweptback wing having an aspect ratio of 3, a taper ratio of 0.2, and NACA 65A004 airfoil sections has been conducted in the Langley16-foot transonic tunnel. Pressure measurements on the wing-body combination were obtained at angles of attack from 0 to 26 degrees at Mach numbers from 0.80 to 0.98 and from 0 to about 12 degrees at Mach numbers from 1.00 to 1.05. Reynolds number, based on the wing mean aerodynamic chord, varied from 7,000,000 to 8,500,000 over the test Mach number range.
Book Synopsis The Effects of an Inverse-taper Leading-edge Flap on the Aerodynamic Loading Characteristics of a 45° Sweptback Wing at Mach Numbers to 0.90 by : Fred A. Demele
Download or read book The Effects of an Inverse-taper Leading-edge Flap on the Aerodynamic Loading Characteristics of a 45° Sweptback Wing at Mach Numbers to 0.90 written by Fred A. Demele and published by . This book was released on 1959 with total page 112 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Effects of Leading-edge Slats on the Aerodynamic Characteristics of a 45 Degree Sweepback Wing-fuselage Configuration at Mach Numbers of 0.4 to 1.03 by : Jack F. Runckel
Download or read book Effects of Leading-edge Slats on the Aerodynamic Characteristics of a 45 Degree Sweepback Wing-fuselage Configuration at Mach Numbers of 0.4 to 1.03 written by Jack F. Runckel and published by . This book was released on 1953 with total page 50 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Theoretical Loading at Supersonic Speeds of Flat Swept-back Wings with Interacting Trailing and Leading Edges by : Doris Cohen
Download or read book Theoretical Loading at Supersonic Speeds of Flat Swept-back Wings with Interacting Trailing and Leading Edges written by Doris Cohen and published by . This book was released on 1949 with total page 64 pages. Available in PDF, EPUB and Kindle. Book excerpt: By the method of superposition of conical flows, the load distribution is calculated for regions of a long swept-back wing behind the points at which the Mach lines from the trailing-edge apex intersect the leading edge. It is found that a good approximation on the load can be obtained by the application of a fairly simple correction factor to the two-dimensional subsonic distribution. The similarity of two-dimensional flow is used to derive expressions for the loss of lift behind the Mach lines from the tips of the wing.
Book Synopsis Aerodynamic Characteristics of a Small-scale Straight and Swept-back Wing with Knee-blown Jet Flaps by :
Download or read book Aerodynamic Characteristics of a Small-scale Straight and Swept-back Wing with Knee-blown Jet Flaps written by and published by . This book was released on 1977 with total page 130 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Wind-tunnel Investigation of Effect of Ratio of Wing Chord to Propeller Diameter with Addition of Slats on the Aerodynamic Characteristics of Tilt-wing VTOL Configurations in the Transition Speed Range by : Robert T. Taylor
Download or read book Wind-tunnel Investigation of Effect of Ratio of Wing Chord to Propeller Diameter with Addition of Slats on the Aerodynamic Characteristics of Tilt-wing VTOL Configurations in the Transition Speed Range written by Robert T. Taylor and published by . This book was released on 1959 with total page 48 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Normal-force and Hinge-moment Characteristics at Transonic Speeds of Flap-type Ailerons at Three Spanwise Locations on a 4-percent-thick Sweptback-wing-body Model and Pressure-distribution Measurements on an Inboard Aileron by : Jack F. Runckel
Download or read book Normal-force and Hinge-moment Characteristics at Transonic Speeds of Flap-type Ailerons at Three Spanwise Locations on a 4-percent-thick Sweptback-wing-body Model and Pressure-distribution Measurements on an Inboard Aileron written by Jack F. Runckel and published by . This book was released on 1961 with total page 60 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Investigation at Transonic Speeds of the Loading Over a 45 Degree Sweptback Wing Having an Aspect Ratio of 3, a Taper Ratio of 0.2, and Naca 65a004 Airfoil Sections by : JACK F. RUNCKEL
Download or read book Investigation at Transonic Speeds of the Loading Over a 45 Degree Sweptback Wing Having an Aspect Ratio of 3, a Taper Ratio of 0.2, and Naca 65a004 Airfoil Sections written by JACK F. RUNCKEL and published by . This book was released on 1961 with total page 1 pages. Available in PDF, EPUB and Kindle. Book excerpt: An investigation at transonic speeds of the loading over a 45 degree sweptback wing having an aspect ratio of 3, a taper ratio of 0.2, and NACA 65A004 airfoil sections was conducted in the Langley 16-foot transonic tunnel. Pressure measurements on the wing-body combi ation were obtained at angles of attack from 0 degrees to 26 degrees at Mach numbers from 0.80 to 0.98 and at angles of attack from 0 degrees to about 12 degrees at Mach numbers from 1.00 to 1.05. Reynolds number, based on the wing mean aerodynamic c ord varied from 7 times 10 to the 6th po er to 8.5 times 10 to the 6th power over the test Mach number range. Results of the investigation indicate that a highly swept shock originates at the juncture of the wing leading edge and the body at moderate angles of attack and has a large influence on the loading over the inboard wing sections. (Author).
