An Experimental Investigation of the Flow Fields about Delta and Double-delta Wings at Low Speeds

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ISBN 13 :
Total Pages : 160 pages
Book Rating : 4.:/5 (317 download)

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Book Synopsis An Experimental Investigation of the Flow Fields about Delta and Double-delta Wings at Low Speeds by : William H. Wentz (Jr.)

Download or read book An Experimental Investigation of the Flow Fields about Delta and Double-delta Wings at Low Speeds written by William H. Wentz (Jr.) and published by . This book was released on 1966 with total page 160 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Further Experimental Investigation of Delta and Double-delta Wing Flow Fields at Low Speeds

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ISBN 13 :
Total Pages : 129 pages
Book Rating : 4.:/5 (254 download)

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Book Synopsis Further Experimental Investigation of Delta and Double-delta Wing Flow Fields at Low Speeds by : William H. Wentz

Download or read book Further Experimental Investigation of Delta and Double-delta Wing Flow Fields at Low Speeds written by William H. Wentz and published by . This book was released on 1967 with total page 129 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Further Experimental Investigations of Delta and Double-delta Wing Flow Fields at Low Speeds

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ISBN 13 :
Total Pages : 140 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis Further Experimental Investigations of Delta and Double-delta Wing Flow Fields at Low Speeds by : W. H. Wentz

Download or read book Further Experimental Investigations of Delta and Double-delta Wing Flow Fields at Low Speeds written by W. H. Wentz and published by . This book was released on 1967 with total page 140 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Tuft-grid Surveys at Low Speeds for Delta Wings

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ISBN 13 :
Total Pages : 44 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis Tuft-grid Surveys at Low Speeds for Delta Wings by : John D. Bird

Download or read book Tuft-grid Surveys at Low Speeds for Delta Wings written by John D. Bird and published by . This book was released on 1968 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt:

An Experimental Investigation of the Flow Fields about Delta and Boubledelta Wings at Low Speeds

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ISBN 13 :
Total Pages : 143 pages
Book Rating : 4.:/5 (889 download)

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Book Synopsis An Experimental Investigation of the Flow Fields about Delta and Boubledelta Wings at Low Speeds by : William H. Wentz

Download or read book An Experimental Investigation of the Flow Fields about Delta and Boubledelta Wings at Low Speeds written by William H. Wentz and published by . This book was released on 1966 with total page 143 pages. Available in PDF, EPUB and Kindle. Book excerpt:

A Note on the Drag Due to Lift of Delta Wings at Mach Numbers Up to 2.0

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ISBN 13 :
Total Pages : 20 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis A Note on the Drag Due to Lift of Delta Wings at Mach Numbers Up to 2.0 by : Robert S. Osborne

Download or read book A Note on the Drag Due to Lift of Delta Wings at Mach Numbers Up to 2.0 written by Robert S. Osborne and published by . This book was released on 1960 with total page 20 pages. Available in PDF, EPUB and Kindle. Book excerpt:

An Experimental Investigation of the Vortex Flow Over Delta and Double-Delta Wings at Low Speed

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ISBN 13 :
Total Pages : 16 pages
Book Rating : 4.:/5 (228 download)

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Book Synopsis An Experimental Investigation of the Vortex Flow Over Delta and Double-Delta Wings at Low Speed by : N. G. Verhaagen

Download or read book An Experimental Investigation of the Vortex Flow Over Delta and Double-Delta Wings at Low Speed written by N. G. Verhaagen and published by . This book was released on 1983 with total page 16 pages. Available in PDF, EPUB and Kindle. Book excerpt: A wind-tunnel investigation was performed to study, by employing a laserlight-sheet and oil-flow visualization technique, the flow above and behind a sharp-edge 76 deg, delta wing and two sharp-edged double-delta wing models (76/60 and 76/40 deg., kink at midcord). In addition, balance measurements were performed to determine lift, drag and pitching moment. The tests were carried out for angles of attack from 5 to 25 deg. and at a free-stream velocity of 30 m/sec, corresponding to a Reynolds number of 1400000 x 10 to the 6th power, based on centerline chord. Above both double-delta wings a single-branched strake vortex is formed fed by vorticity from the strake leading edge. Downstream of the leading-edge kink a wing vortex is formed which is conjectured to be single-branched at about 5 deg, angle of attack and double branched at angles of 10 deg., an beyond. The flow pattern downstream of the trailing edge of the 76/60 deg. double-delta wing has been observed to be similar to that behind the delta wing. Above the 76/40 deg. double-delta wing breakdown of both the wing and strake vortices took place ahead of the trailing edge. (Author).

Investigation of Leading-edge Flap Performance on Delta and Double-delta Wings at Supersonic Speeds

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ISBN 13 :
Total Pages : 132 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis Investigation of Leading-edge Flap Performance on Delta and Double-delta Wings at Supersonic Speeds by : Peter F. Covell

Download or read book Investigation of Leading-edge Flap Performance on Delta and Double-delta Wings at Supersonic Speeds written by Peter F. Covell and published by . This book was released on 1987 with total page 132 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Detailed Flow-field Measurements Over a 75 ̊swept Delta Wing

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ISBN 13 :
Total Pages : 52 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis Detailed Flow-field Measurements Over a 75 ̊swept Delta Wing by : Scott O. Kjelgaard

Download or read book Detailed Flow-field Measurements Over a 75 ̊swept Delta Wing written by Scott O. Kjelgaard and published by . This book was released on 1990 with total page 52 pages. Available in PDF, EPUB and Kindle. Book excerpt:

An Experimental Investigation of Leading Edge Vortices and Passage to Stall of Nonslender Delta Wings

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ISBN 13 :
Total Pages : 17 pages
Book Rating : 4.:/5 (742 download)

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Book Synopsis An Experimental Investigation of Leading Edge Vortices and Passage to Stall of Nonslender Delta Wings by :

Download or read book An Experimental Investigation of Leading Edge Vortices and Passage to Stall of Nonslender Delta Wings written by and published by . This book was released on 2003 with total page 17 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Swept and Delta Wing Sense

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ISBN 13 :
Total Pages : 44 pages
Book Rating : 4.E/5 ( download)

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Book Synopsis Swept and Delta Wing Sense by :

Download or read book Swept and Delta Wing Sense written by and published by . This book was released on 1955 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Investigation of Leading-edge Flap Performance on Delta and Double-delta Wings at Supersonic Speeds

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ISBN 13 :
Total Pages : 132 pages
Book Rating : 4.:/5 (317 download)

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Book Synopsis Investigation of Leading-edge Flap Performance on Delta and Double-delta Wings at Supersonic Speeds by : Peter F. Covell

Download or read book Investigation of Leading-edge Flap Performance on Delta and Double-delta Wings at Supersonic Speeds written by Peter F. Covell and published by . This book was released on 1987 with total page 132 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Lee-side Flow Over Delta Wings at Supersonic Speeds

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ISBN 13 :
Total Pages : 160 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis Lee-side Flow Over Delta Wings at Supersonic Speeds by : David S. Miller

Download or read book Lee-side Flow Over Delta Wings at Supersonic Speeds written by David S. Miller and published by . This book was released on 1985 with total page 160 pages. Available in PDF, EPUB and Kindle. Book excerpt:

An Experimental Study of the Flow Field about Swept and Delta Wings with Sharp Leading Edges

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ISBN 13 :
Total Pages : 22 pages
Book Rating : 4.:/5 (977 download)

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Book Synopsis An Experimental Study of the Flow Field about Swept and Delta Wings with Sharp Leading Edges by : Ivan Jaszlics

Download or read book An Experimental Study of the Flow Field about Swept and Delta Wings with Sharp Leading Edges written by Ivan Jaszlics and published by . This book was released on 1957 with total page 22 pages. Available in PDF, EPUB and Kindle. Book excerpt:

An Experimental Investigation of Incompressible Flow Over Delta and Double-Delta Wings

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ISBN 13 :
Total Pages : 79 pages
Book Rating : 4.:/5 (227 download)

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Book Synopsis An Experimental Investigation of Incompressible Flow Over Delta and Double-Delta Wings by : James K. Nathman

Download or read book An Experimental Investigation of Incompressible Flow Over Delta and Double-Delta Wings written by James K. Nathman and published by . This book was released on 1976 with total page 79 pages. Available in PDF, EPUB and Kindle. Book excerpt: An experimental study of the flow over delta and double-delta wings was conducted in a 7' x 10' low speed wing tunnel. The configurations tested were AR-3 and AR-4 delta wings and the AR-4 wing which was modified with AR-1 and AR-2 strakes attached to form double-delta wings. Pressure measurements, surface flow visualization, and vortex core visualization studies were conducted over a wide range of angles of attack.

An Experimental Investigation of Buffeting Flows Over Delta Wings

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ISBN 13 :
Total Pages : 214 pages
Book Rating : 4.:/5 (419 download)

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Book Synopsis An Experimental Investigation of Buffeting Flows Over Delta Wings by : Wensheng Xie

Download or read book An Experimental Investigation of Buffeting Flows Over Delta Wings written by Wensheng Xie and published by . This book was released on 1998 with total page 214 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Flow Field Over the Wing of a Delta-wing Fighter Model with Vortex Control Devices at Mach 0.6 to 1.2

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ISBN 13 :
Total Pages : 132 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis Flow Field Over the Wing of a Delta-wing Fighter Model with Vortex Control Devices at Mach 0.6 to 1.2 by : E. Ann Bare

Download or read book Flow Field Over the Wing of a Delta-wing Fighter Model with Vortex Control Devices at Mach 0.6 to 1.2 written by E. Ann Bare and published by . This book was released on 1992 with total page 132 pages. Available in PDF, EPUB and Kindle. Book excerpt: