Related Books

Investigation of Drag Reduction by Boundary Layer Suction on a 50-deg Swept Tapered Wing at M (free-stream)
Language: en
Pages: 32

Investigation of Drag Reduction by Boundary Layer Suction on a 50-deg Swept Tapered Wing at M (free-stream)

Authors: S. R. Pate
Categories: Airplanes
Type: BOOK - Published: 1964 - Publisher:

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Tests were conducted in the 40-in. supersonic Tunnel A of the von Karman Gas Dynamics Facility to determine the effectiveness of boundary layer suction for lami
Investigation of Drag Reduction by Boundarylayer Suction on a 50-degree Swept Tapered Wing at M (free-stream) Equals 2.5 to 4
Language: en
Pages: 31

Investigation of Drag Reduction by Boundarylayer Suction on a 50-degree Swept Tapered Wing at M (free-stream) Equals 2.5 to 4

Authors: S. R. Pate
Categories:
Type: BOOK - Published: 1964 - Publisher:

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Tests were conducted in the 40-in. supersonic Tunnel A of the von Karman Gas Dynamics Facility to determine the effectiveness of boundarylayer suction for lamin
Investigation of Drag Reduction by Boundary-layer Suction on a Flat Plate and a 36-deg Swept Wing at Supersonic Speeds
Language: en
Pages: 46

Investigation of Drag Reduction by Boundary-layer Suction on a Flat Plate and a 36-deg Swept Wing at Supersonic Speeds

Authors: S. R. Pate
Categories: Aerodynamics, Supersonic
Type: BOOK - Published: 1962 - Publisher:

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Tests were conducted in a 40-in. supersonic tunnel to determine the effectiveness of boundary-layer suction for laminar flow control on a two-dimensional, bicon
Investigation of Drag Reduction by Boundary Layer Suction on a 72.5-deg Swept Wind at M 2 and 2.25
Language: en
Pages: 27

Investigation of Drag Reduction by Boundary Layer Suction on a 72.5-deg Swept Wind at M 2 and 2.25

Authors: S. R. Pate
Categories:
Type: BOOK - Published: 1963 - Publisher:

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Tests were conducted in the 40-Inch Supersonic Tunnel (A) of the von Karman Gas Dynamics Facility to determine the effectiveness of boundary layer suction for l
An Experimental Investigation of Boundary-layer Control for Drag Reduction of a Swept-wing Section at Low Speed and High Reynolds Numbers
Language: en
Pages: 22

An Experimental Investigation of Boundary-layer Control for Drag Reduction of a Swept-wing Section at Low Speed and High Reynolds Numbers

Authors: Donald E. Gault
Categories: Aerodynamics
Type: BOOK - Published: 1960 - Publisher:

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