Slats

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 : Dirk Barreveld
Publisher : Lulu.com
ISBN 13 : 1329720024
Total Pages : 99 pages
Book Rating : 4.22/5 ( download)

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Download or read book AIR CRASH INVESTIGATIONS - Inadvertent In-Flight Slat Deployment - The Near Crash of China Eastern Airlines Flight 583 written by Dirk Barreveld and published by Lulu.com. This book was released on 2015-11-28 with total page 99 pages. Available in PDF, EPUB and Kindle. Book excerpt: On April 6, 1993, a China Eastern Airlines McDonnell Douglas MD-11, flight 583, on its way from Beijing, China, to Los Angeles, California, had an inadvertent deployment of the leading edge wing slats while in cruise flight, not far from Shemya, Alaska. The autopilot disconnected, and the captain was manually controlling the airplane when it progressed through several violent pitch oscillations and lost 5,000 feet of altitude. Two passengers were fatally injured, and 149 passengers and 7 crewmembers received various injuries. The airplane did not receive external structural damage, but the passenger cabin was substantially damaged. The National Transportation Safety Board determined that the probable cause of this accident was the inadequate design of the flap/slat actuation handle by the Douglas Aircraft Company that allowed the handle to be easily and inadvertently dislodged from the UP/RET position, thereby causing extension of the leading edge slats during cruise flight.

Author : Gene J. Matranga
Publisher :
ISBN 13 :
Total Pages : 50 pages
Book Rating : 4.30/5 ( download)

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Download or read book Flight Evaluation of the Effects of Leading-edge-slat Span on the Stability and Control Characteristics of a Swept-wing Fighter-type Airplane During Accelerated Longitudinal Maneuvers at Transonic Speeds written by Gene J. Matranga and published by . This book was released on 1958 with total page 50 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Author : United States. National Bureau of Standards
Publisher :
ISBN 13 :
Total Pages : 16 pages
Book Rating : 4.83/5 ( download)

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Download or read book Mosaic-parquet Hardwood Slat Flooring written by United States. National Bureau of Standards and published by . This book was released on 1970 with total page 16 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Author : Canada. Patent Office
Publisher :
ISBN 13 :
Total Pages : 1420 pages
Book Rating : 4.96/5 ( download)

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Download or read book Scientific Canadian Mechanics' Magazine and Patent Office Record written by Canada. Patent Office and published by . This book was released on 1894 with total page 1420 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 : John A. Axelson
Publisher :
ISBN 13 :
Total Pages : 696 pages
Book Rating : 4.33/5 ( download)

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Download or read book Investigation of a Slat in Several Different Positions on an NACA 64A010 Airfoil for a Wide Range of Subsonic Mach Numbers written by John A. Axelson and published by . This book was released on 1954 with total page 696 pages. Available in PDF, EPUB and Kindle. Book excerpt: An investigation of the two-dimensional aerodynamic characteristics of an NACA 64A010 airfoil with a slat has been conducted in the Mach number range from 0.25 to 0.85, with a corresponding Reynolds number range from 3.4 million to 8.1 million. Two families of slat positions were investigated, one with the slat leading edge extended forward along the airfoil chord line, and the other with the slat extended forward and displaced below the chord line.

Author : United States. Patent Office
Publisher :
ISBN 13 :
Total Pages : 1494 pages
Book Rating : 4.64/5 ( download)

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Download or read book Official Gazette of the United States Patent Office written by United States. Patent Office and published by . This book was released on 1888 with total page 1494 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Author : United States. Patent Office
Publisher :
ISBN 13 :
Total Pages : 1232 pages
Book Rating : 4.53/5 ( download)

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Download or read book Specifications and Drawings of Patents Issued from the U.S. Patent Office written by United States. Patent Office and published by . This book was released on 1873 with total page 1232 pages. Available in PDF, EPUB and Kindle. Book excerpt: