Slats

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

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Author : Donald D. Arabian
language : en
Publisher:
Release Date : 1954

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 has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1954 with Airplanes categories.

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

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Author : Donald D. Arabian
language : en
Publisher:
Release Date : 1961

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 has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1961 with Airplanes categories.

Air Crash Investigations Inadvertent In Flight Slat Deployment The Near Crash Of China Eastern Airlines Flight 583

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Author : Dirk Barreveld
language : en
Publisher: Lulu.com
Release Date : 2015-11-28

Air Crash Investigations Inadvertent In Flight Slat Deployment The Near Crash Of China Eastern Airlines Flight 583 written by Dirk Barreveld and has been published by Lulu.com this book supported file pdf, txt, epub, kindle and other format this book has been release on 2015-11-28 with History categories.

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.

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

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Author : Gene J. Matranga
language : en
Publisher:
Release Date : 1958

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 has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1958 with Fighter planes categories.

Mosaic Parquet Hardwood Slat Flooring

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Author : United States. National Bureau of Standards
language : en
Publisher:
Release Date : 1970

Mosaic Parquet Hardwood Slat Flooring written by United States. National Bureau of Standards and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1970 with Parquet floors categories.

Aerodynamic Characteristics Of A Leading Edge Slat On A 35 Degree Swept Back Wing For Mach Numbers From 0 30 To 0 88

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Author : John A. Kelly
language : en
Publisher:
Release Date : 1951

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 has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1951 with Aerodynamic load categories.

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.

Investigation Of A Slat In Several Different Positions On An Naca 64a010 Airfoil For A Wide Range Of Subsonic Mach Numbers

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Author : John A. Axelson
language : en
Publisher:
Release Date : 1954

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 has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1954 with Aerodynamics categories.

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.

Official Gazette Of The United States Patent Office

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Author : United States. Patent Office
language : en
Publisher:
Release Date : 1899

Official Gazette Of The United States Patent Office written by United States. Patent Office and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1899 with Patents categories.

Scientific Canadian Mechanics Magazine And Patent Office Record

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Author : Canada. Patent Office
language : en
Publisher:
Release Date : 1894

Scientific Canadian Mechanics Magazine And Patent Office Record written by Canada. Patent Office and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1894 with Copyright categories.

Specifications And Drawings Of Patents Issued From The U S Patent Office

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Author : United States. Patent Office
language : en
Publisher:
Release Date : 1873

Specifications And Drawings Of Patents Issued From The U S Patent Office written by United States. Patent Office and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1873 with categories.