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Production at the Leading Edge of Technology
Language: en
Pages: 693

Production at the Leading Edge of Technology

Authors: Bernd-Arno Behrens
Categories: Technology & Engineering
Type: BOOK - Published: 2021-09-04 - Publisher: Springer Nature

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This congress proceedings provides recent research on leading-edge manufacturing processes. The aim of this scientific congress is to work out diverse individua
Wind-tunnel and Flight Investigations of the Use of Leading-edge Area Suction for the Purpose of Increasing the Maximum Lift Coefficient of a 35 ̊swept-wing Airplane
Language: en
Pages: 284

Wind-tunnel and Flight Investigations of the Use of Leading-edge Area Suction for the Purpose of Increasing the Maximum Lift Coefficient of a 35 ̊swept-wing Airplane

Authors: Curt A. Holzhauer
Categories: Aerofoils
Type: BOOK - Published: 1956 - Publisher:

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Flight Tests of a Leading-edge Area Suction on a Fighter-type Airplane with a 35 Degree Sweptback Wing
Language: en
Pages: 34

Flight Tests of a Leading-edge Area Suction on a Fighter-type Airplane with a 35 Degree Sweptback Wing

Authors: Richard S. Bray
Categories: Aeronautics
Type: BOOK - Published: 1955 - Publisher:

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Tests have been made to determine the flight characteristics of an F-86F airplane equipped with a leading-edge area-suction boundary-layer-control system, and t
Effect of Leading-edge Thickness on the Flow Over a Flat Plate at a Mach Number of 5.7
Language: en
Pages: 36

Effect of Leading-edge Thickness on the Flow Over a Flat Plate at a Mach Number of 5.7

Authors: Marcus O. Creager
Categories: Aerodynamics, Hypersonic
Type: BOOK - Published: 1960 - Publisher:

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Investigation of the Effects of Leading-edge Chord-extensions and Fences in Combination with Leading-edge Flaps on the Aerodynamic Characteristics at Mach Numbers from 0.40 to 0.93 of a 45 Degree Sweptback Wing of Aspect Ratio 4
Language: en
Pages: 644

Investigation of the Effects of Leading-edge Chord-extensions and Fences in Combination with Leading-edge Flaps on the Aerodynamic Characteristics at Mach Numbers from 0.40 to 0.93 of a 45 Degree Sweptback Wing of Aspect Ratio 4

Authors: Kenneth P. Spreemann
Categories: Airplanes
Type: BOOK - Published: 1957 - Publisher:

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This investigation was made to determine the effects of 6 degree full-span and 3 degree partial-span leading-edge flaps in combination with chord-extensions or