A Wind-tunnel Investigation of a 4-foot-diameter Ducted Fan Mounted on the Tip of a Semispan Wing

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ISBN 13 :
Total Pages : 36 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis A Wind-tunnel Investigation of a 4-foot-diameter Ducted Fan Mounted on the Tip of a Semispan Wing by : Paul F. Yaggy

Download or read book A Wind-tunnel Investigation of a 4-foot-diameter Ducted Fan Mounted on the Tip of a Semispan Wing written by Paul F. Yaggy and published by . This book was released on 1961 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Wind-tunnel Investigation of a Revised Horizontal Tail Surface for the Grumman TBF-1 Airplane

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Publisher :
ISBN 13 :
Total Pages : 50 pages
Book Rating : 4.3/5 (91 download)

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Book Synopsis Wind-tunnel Investigation of a Revised Horizontal Tail Surface for the Grumman TBF-1 Airplane by : John W. McKee

Download or read book Wind-tunnel Investigation of a Revised Horizontal Tail Surface for the Grumman TBF-1 Airplane written by John W. McKee and published by . This book was released on 1943 with total page 50 pages. Available in PDF, EPUB and Kindle. Book excerpt: An investigation was made in the LMAL 7- by 10-foot tunnel of the aerodynamic characteristics of a revised 0.5-scale model of the Grumman TBF-1 left horizontal tail surface. The investigation was undertaken to determine if a horizontal tail surface with a large overhang would reduce the high stick forces in maneuvers that the airplane had with the original horn-balanced elevator, without appreciably affecting the longitudinal stability characteristics of the airplane.

Wind Tunnel Investigation of Control Surface Characteristics

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Publisher :
ISBN 13 :
Total Pages : 42 pages
Book Rating : 4.3/5 (91 download)

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Book Synopsis Wind Tunnel Investigation of Control Surface Characteristics by : H. Page Hoggard

Download or read book Wind Tunnel Investigation of Control Surface Characteristics written by H. Page Hoggard and published by . This book was released on 1943 with total page 42 pages. Available in PDF, EPUB and Kindle. Book excerpt: Force-test measurements in two-dimensional flow have been made in the NACA 4- by 6-foot vertical tunnel to determine the aerodynamic effects of changing the alignment of the cover plates on a sealed internally balanced flap. An NACA 0015 airfoil was utilized for the tests. The chord of the straight-contour flap was 30 percent of the airfoil chord and the balance with 50 percent of the flap chord.

Longitudinal Airplane Dynamics Wind Tunnel Test Equipment

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Publisher :
ISBN 13 :
Total Pages : 246 pages
Book Rating : 4.3/5 (91 download)

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Book Synopsis Longitudinal Airplane Dynamics Wind Tunnel Test Equipment by : O. B. Tufts

Download or read book Longitudinal Airplane Dynamics Wind Tunnel Test Equipment written by O. B. Tufts and published by . This book was released on 1955 with total page 246 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Wind-tunnel Investigation of Rounded Horns and of Guards on a Horizontal Tail Surface

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Publisher :
ISBN 13 :
Total Pages : 124 pages
Book Rating : 4.3/5 (126 download)

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Book Synopsis Wind-tunnel Investigation of Rounded Horns and of Guards on a Horizontal Tail Surface by : Robert B. Liddell

Download or read book Wind-tunnel Investigation of Rounded Horns and of Guards on a Horizontal Tail Surface written by Robert B. Liddell and published by . This book was released on 1944 with total page 124 pages. Available in PDF, EPUB and Kindle. Book excerpt: Summary: An investigation was made to determine the aerodynamic effects of horn balances with various plan forms and of guards on a horizontal tail surface. The results indicate that rounding the adjacent horn and stabilizer edges caused neglibible changes in the aerodynamic characteristics, except for the changes resulting from the decrease in the area momeent of the horn. The use of guards mounted between the stabilizer and horn was found to increase the slope of the lift curves with angle of attack or with elevator deflection. The negative slopes of the curves of hinge moment against angle of attack and elevator deflection increased as the guard area was increased.

Wind Tunnel Tests on Airfoil Boundary Layer Control Using a Backward-opening Slot

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Publisher :
ISBN 13 :
Total Pages : 160 pages
Book Rating : 4.3/5 (243 download)

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Book Synopsis Wind Tunnel Tests on Airfoil Boundary Layer Control Using a Backward-opening Slot by : C. H. Dearborn

Download or read book Wind Tunnel Tests on Airfoil Boundary Layer Control Using a Backward-opening Slot written by C. H. Dearborn and published by . This book was released on 1931 with total page 160 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Transonic Wind-tunnel Investigation of the Interference Between a 45© Sweptback Wing and a Systematic Series of Four Bodies

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Publisher :
ISBN 13 :
Total Pages : 52 pages
Book Rating : 4.3/5 (91 download)

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Book Synopsis Transonic Wind-tunnel Investigation of the Interference Between a 45© Sweptback Wing and a Systematic Series of Four Bodies by : Donald L. Loving

Download or read book Transonic Wind-tunnel Investigation of the Interference Between a 45© Sweptback Wing and a Systematic Series of Four Bodies written by Donald L. Loving and published by . This book was released on 1952 with total page 52 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Tests of Submerged Duct Installation on a Modified Fighter Airplane in the Ames 40- by 80-foot Wind Tunnel

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Publisher :
ISBN 13 :
Total Pages : 32 pages
Book Rating : 4.3/5 (91 download)

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Book Synopsis Tests of Submerged Duct Installation on a Modified Fighter Airplane in the Ames 40- by 80-foot Wind Tunnel by : Norman J. Martin

Download or read book Tests of Submerged Duct Installation on a Modified Fighter Airplane in the Ames 40- by 80-foot Wind Tunnel written by Norman J. Martin and published by . This book was released on 1947 with total page 32 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Wind Tunnel Investigation of Effect of Yaw on Lateral-stability Characteristics

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Publisher :
ISBN 13 :
Total Pages : 36 pages
Book Rating : 4.3/5 (91 download)

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Book Synopsis Wind Tunnel Investigation of Effect of Yaw on Lateral-stability Characteristics by : Isidore G. Recant

Download or read book Wind Tunnel Investigation of Effect of Yaw on Lateral-stability Characteristics written by Isidore G. Recant and published by . This book was released on 1942 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt: Combinations of an NACA 23012 tapered wing and a circular fuselage having a wedge-shaped rear were tested in the NACA 7- by 10-foot wind tunnel to determine the effect of wing-fuselage interference on the lateral-stability of wing-fuselage interference on the lateral-stability characteristics. The model configurations represented a high-wing, a mid-wing, and a low-wing monoplane. For each configuration, tests were made with a partial-span split flap neutral and deflected 60 degrees and with and without a vertical tail. Tests of the fuselage alone and of the fuselage with the vertical tail were also made.

Wind-tunnel Investigation of Control-surface Characteristics.

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Publisher : Hassell Street Press
ISBN 13 : 9781014860965
Total Pages : 96 pages
Book Rating : 4.8/5 (69 download)

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Book Synopsis Wind-tunnel Investigation of Control-surface Characteristics. by : Langley Aeronautical Laboratory

Download or read book Wind-tunnel Investigation of Control-surface Characteristics. written by Langley Aeronautical Laboratory and published by Hassell Street Press. This book was released on 2021-09-09 with total page 96 pages. Available in PDF, EPUB and Kindle. Book excerpt: This work has been selected by scholars as being culturally important and is part of the knowledge base of civilization as we know it. This work is in the public domain in the United States of America, and possibly other nations. Within the United States, you may freely copy and distribute this work, as no entity (individual or corporate) has a copyright on the body of the work. Scholars believe, and we concur, that this work is important enough to be preserved, reproduced, and made generally available to the public. To ensure a quality reading experience, this work has been proofread and republished using a format that seamlessly blends the original graphical elements with text in an easy-to-read typeface. We appreciate your support of the preservation process, and thank you for being an important part of keeping this knowledge alive and relevant.

Measurements of Section Characteristics of a 45 Degree Swept Wing Spanning a Rectangular Low-speed Wind Tunnel as Affected by the Tunnel Walls

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Publisher :
ISBN 13 :
Total Pages : 678 pages
Book Rating : 4.F/5 ( download)

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Book Synopsis Measurements of Section Characteristics of a 45 Degree Swept Wing Spanning a Rectangular Low-speed Wind Tunnel as Affected by the Tunnel Walls by : Robert E. Dannenberg

Download or read book Measurements of Section Characteristics of a 45 Degree Swept Wing Spanning a Rectangular Low-speed Wind Tunnel as Affected by the Tunnel Walls written by Robert E. Dannenberg and published by . This book was released on 1950 with total page 678 pages. Available in PDF, EPUB and Kindle. Book excerpt: Tunnel-wall corrections for the induced upwash velocity for a swept wing completely spanning a rectangular wind tunnel are included in the appendix.

Wall Interference in Wind Tunnels with Slotted and Porous Boundaries at Subsonic Speeds

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Publisher :
ISBN 13 :
Total Pages : 46 pages
Book Rating : 4.3/5 (91 download)

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Book Synopsis Wall Interference in Wind Tunnels with Slotted and Porous Boundaries at Subsonic Speeds by : Barrett Stone Baldwin

Download or read book Wall Interference in Wind Tunnels with Slotted and Porous Boundaries at Subsonic Speeds written by Barrett Stone Baldwin and published by . This book was released on 1953 with total page 46 pages. Available in PDF, EPUB and Kindle. Book excerpt: Linearized compressible-flow analysis is applied to the study of wind-tunnel-wall interference for subsonic flow in either two-dimensional or circular test sections having slotted or porous walls. Expressions are developed for evaluating blockage and lift interference.

Wind Tunnel Investigation of Three Axisymmetric Cowls of Different Lengths at Mach Numbers from 0.60 to 0.92

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Publisher :
ISBN 13 :
Total Pages : 292 pages
Book Rating : 4.:/5 (317 download)

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Book Synopsis Wind Tunnel Investigation of Three Axisymmetric Cowls of Different Lengths at Mach Numbers from 0.60 to 0.92 by : Richard J. Re

Download or read book Wind Tunnel Investigation of Three Axisymmetric Cowls of Different Lengths at Mach Numbers from 0.60 to 0.92 written by Richard J. Re and published by . This book was released on 1993 with total page 292 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Low-Speed Wind Tunnel Testing

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Publisher : Wiley-Interscience
ISBN 13 :
Total Pages : 562 pages
Book Rating : 4.3/5 (91 download)

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Book Synopsis Low-Speed Wind Tunnel Testing by : Alan Pope

Download or read book Low-Speed Wind Tunnel Testing written by Alan Pope and published by Wiley-Interscience. This book was released on 1984 with total page 562 pages. Available in PDF, EPUB and Kindle. Book excerpt: Good,No Highlights,No Markup,all pages are intact, Slight Shelfwear,may have the corners slightly dented, may have slight color changes/slightly damaged spine.

The Generation of Gusts in a Wind Tunnel and Measurement of Unsteady Lift on an Airfoil

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Publisher :
ISBN 13 :
Total Pages : 56 pages
Book Rating : 4.3/5 (91 download)

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Book Synopsis The Generation of Gusts in a Wind Tunnel and Measurement of Unsteady Lift on an Airfoil by : L. C. Garby

Download or read book The Generation of Gusts in a Wind Tunnel and Measurement of Unsteady Lift on an Airfoil written by L. C. Garby and published by . This book was released on 1957 with total page 56 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Wind Tunnels

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Publisher : BoD – Books on Demand
ISBN 13 : 9533072954
Total Pages : 150 pages
Book Rating : 4.5/5 (33 download)

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Book Synopsis Wind Tunnels by : Satoru Okamoto

Download or read book Wind Tunnels written by Satoru Okamoto and published by BoD – Books on Demand. This book was released on 2011-02-10 with total page 150 pages. Available in PDF, EPUB and Kindle. Book excerpt: Although great advances in computational methods have been made in recent years, wind tunnel tests remain essential for obtaining the full range of data required to guide detailed design decisions for various practical engineering problems. This book collects original and innovative research studies on recent applications in wind tunnel tests, exhibiting various investigation directions and providing a bird’s eye view on this broad subject area. It is composed of seven chapters that have been grouped in two major parts. The first part of the book (chapters 1–4) deals with wind tunnel technologies and devices. The second part (chapters 5–7) deals with the latest applications of wind tunnel testing. The text is addressed not only to researchers but also to professional engineers, engineering lecturers, and students seeking to gain better understanding of the current status of wind tunnels. Through its seven chapters, the reader will have an access to a wide range of works related to wind tunnel testing.

Wind-tunnel Studies at Subsonic and Transonic Speeds of a Multiple-mission Variable-wing- Sweep Airplane Configuration

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Publisher :
ISBN 13 :
Total Pages : 82 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis Wind-tunnel Studies at Subsonic and Transonic Speeds of a Multiple-mission Variable-wing- Sweep Airplane Configuration by : William J. Alford

Download or read book Wind-tunnel Studies at Subsonic and Transonic Speeds of a Multiple-mission Variable-wing- Sweep Airplane Configuration written by William J. Alford and published by . This book was released on 1959 with total page 82 pages. Available in PDF, EPUB and Kindle. Book excerpt: