Aerodynamic Load Measurements And Opening Characteristics Of Automatic Leading Edge Slats On A 45c Sweptback Wing At Transonic Speeds

Author : Donald D. Arabian
Publisher :
ISBN 13 :
Total Pages : 54 pages
Book Rating : 4.92/5 ( download)

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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 1954 with total page 54 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Author : Donald D. Arabian
Publisher :
ISBN 13 :
Total Pages : 54 pages
Book Rating : 4.05/5 ( download)

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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:

Author : Donald D. Arabian
Publisher :
ISBN 13 :
Total Pages : 49 pages
Book Rating : 4.96/5 ( download)

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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:

Author : John A. Kelly
Publisher :
ISBN 13 :
Total Pages : 56 pages
Book Rating : 4.71/5 ( download)

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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.

Author : William C. Sleeman
Publisher :
ISBN 13 :
Total Pages : 34 pages
Book Rating : 4.03/5 ( download)

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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.

Author : James W. Schmeer
Publisher :
ISBN 13 :
Total Pages : 42 pages
Book Rating : 4.53/5 ( download)

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Download or read book The Effect of Leading-edge Droop Upon the Pressure Distribution and Aerodynamic Loading Characteristics of a 45 Degree Sweptback Wing at Transonic Speeds written by James W. Schmeer and published by . This book was released on 1955 with total page 42 pages. Available in PDF, EPUB and Kindle. Book excerpt: An investigation was conducted in the Langley 16-foot transonic tunnel to determine the effects of leading-edge droop on the pressure distribution on a 45 degree sweptback wing with an aspect ratio of 4, a taper ratio of 0.6, and NACA 65A006 airfoil sections parallel to the plane of symmetry. The leading edge of the wing was drooped 6 degrees about the 19-percent chord line from 0.15 semispan to the wing tip. Data were obtained at Mach numbers of 0.80 to 1.03 with average Reynolds numbers of 5,700,000 to 6,300,000, respectively. The results of this investigation are compared with the pressure data obtained with the undrooped or basic wing of a previous investigation.

Author : John A. Kelly
Publisher :
ISBN 13 :
Total Pages : 706 pages
Book Rating : 4.49/5 ( download)

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Download or read book Aerodynamic Loads on a Leading-edge Flap and a Leading-edge Slat on the NACA 64A010 Airfoil Section written by John A. Kelly and published by . This book was released on 1954 with total page 706 pages. Available in PDF, EPUB and Kindle. Book excerpt: A previous report, NACA TN 3007, gave force and moment data for the NACA 64A010 airfoil section equipped alternately with a flap and a slat at the leading edge, and with a split flap and a double-slotted flap at the trailing edge. The present report presents the chordwise distributions of pressure measured concurrently with the force and moment data of NACA 3007. The pressure data for the leading-edge flap and slat have been converted into coefficients of normal force, chord force, and moment based on the geometry of the leading-edge device.

Author : Jones F. Cahill
Publisher :
ISBN 13 :
Total Pages : 32 pages
Book Rating : 4.03/5 ( download)

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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:

Author :
Publisher :
ISBN 13 :
Total Pages : 130 pages
Book Rating : 4.70/5 ( download)

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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:

Author : Kenneth P. Spreemann
Publisher :
ISBN 13 :
Total Pages : 56 pages
Book Rating : 4.82/5 ( download)

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Download or read book Investigation of the Effects of Leading-edge Chord-extensions and Fences in Combination with Leading-edge Flaps on the Aerodynamic Characteristics at Mach Numbers of 0.40 to 0.93 of a 45© Sweptback Wing of Aspect Ratio 4 written by Kenneth P. Spreemann and published by . This book was released on 1957 with total page 56 pages. Available in PDF, EPUB and Kindle. Book excerpt: