Aerodynamic Characteristics of Low-aspect-ratio Wings in Close Proximity to the Ground

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

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Book Synopsis Aerodynamic Characteristics of Low-aspect-ratio Wings in Close Proximity to the Ground by : Marvin P. Fink

Download or read book Aerodynamic Characteristics of Low-aspect-ratio Wings in Close Proximity to the Ground written by Marvin P. Fink and published by . This book was released on 1961 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Aerodynamic Characteristics of Low-aspect-ratio Wings in Close Proximity to the Ground

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ISBN 13 :
Total Pages : 1 pages
Book Rating : 4.:/5 (227 download)

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Book Synopsis Aerodynamic Characteristics of Low-aspect-ratio Wings in Close Proximity to the Ground by : Marvin P. Fink

Download or read book Aerodynamic Characteristics of Low-aspect-ratio Wings in Close Proximity to the Ground written by Marvin P. Fink and published by . This book was released on 1961 with total page 1 pages. Available in PDF, EPUB and Kindle. Book excerpt: A wind-tunnel investigation has been conducted to determine the effect of ground proximity on the aerodynamic characteristics of thick highly cambered rectangular wings with aspect ratios of 1, 2, 4, and 6. The results showed that, for these aspect ratios, as the ground was approached all wings experienced increases in lift-curve slope and reductions in induced drag which resulted in increases in lift-drag ratio. Although an increase in lift-curve slope was obtained for all aspect ratios as the ground was approached, the lift coefficient at an angle of attack of 0 degrees for any given aspect ratio remained nearly constant. The experimental results were in general agreement with Wieselsberger's ground-effect theory. As the wings approached the ground, there was an increase in static longitudinal stability at positive angles of attack. When operating in ground effect, all the wings had stability of height at positive angles of attack and instability of height at negative angles of attack. Wing-tip fairings on the wings with aspect ratios of 1 and 2 produced small increases in lift-drag ratio in ground effect. (Author).

Effects of Ground Proximity on the Longitudinal Aerodynamic Characteristics of an Unswept Aspect-ratio-10 Wing

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ISBN 13 :
Total Pages : 68 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis Effects of Ground Proximity on the Longitudinal Aerodynamic Characteristics of an Unswept Aspect-ratio-10 Wing by : Arthur W. Carter

Download or read book Effects of Ground Proximity on the Longitudinal Aerodynamic Characteristics of an Unswept Aspect-ratio-10 Wing written by Arthur W. Carter and published by . This book was released on 1970 with total page 68 pages. Available in PDF, EPUB and Kindle. Book excerpt: Ground proximity effects of unswept aspect ratio 10 wing on longitudinal aerodynamic characteristics.

Powered Low-aspect-ratio Wing In Ground Effect (WIG) Aerodynamic Characteristics

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ISBN 13 :
Total Pages : 56 pages
Book Rating : 4.:/5 (317 download)

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Book Synopsis Powered Low-aspect-ratio Wing In Ground Effect (WIG) Aerodynamic Characteristics by : James L. Thomas

Download or read book Powered Low-aspect-ratio Wing In Ground Effect (WIG) Aerodynamic Characteristics written by James L. Thomas and published by . This book was released on 1979 with total page 56 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Effect of Ground Proximity on the Longitudinal Aerodynamic Characteristics of an Aspect-ratio-1 Wing with and Without Wing-tip Blowing

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ISBN 13 :
Total Pages : 60 pages
Book Rating : 4.F/5 ( download)

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Book Synopsis Effect of Ground Proximity on the Longitudinal Aerodynamic Characteristics of an Aspect-ratio-1 Wing with and Without Wing-tip Blowing by : Raymond E. Mineck

Download or read book Effect of Ground Proximity on the Longitudinal Aerodynamic Characteristics of an Aspect-ratio-1 Wing with and Without Wing-tip Blowing written by Raymond E. Mineck and published by . This book was released on 1974 with total page 60 pages. Available in PDF, EPUB and Kindle. Book excerpt:

A Wind Tunnel Investigation of Ground Effect on the Aerodynamic Characteristics of Low Aspect Ratio Wings

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

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Book Synopsis A Wind Tunnel Investigation of Ground Effect on the Aerodynamic Characteristics of Low Aspect Ratio Wings by : George Lewis Florman (CAPT, USAF.)

Download or read book A Wind Tunnel Investigation of Ground Effect on the Aerodynamic Characteristics of Low Aspect Ratio Wings written by George Lewis Florman (CAPT, USAF.) and published by . This book was released on 1962 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:

Low-speed Longitudinal Aerodynamic Characteristics Associated with a Series of Low-aspect-ration Wings Having Variations in Leading Contour

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ISBN 13 :
Total Pages : 92 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis Low-speed Longitudinal Aerodynamic Characteristics Associated with a Series of Low-aspect-ration Wings Having Variations in Leading Contour by : Bernard Spencer

Download or read book Low-speed Longitudinal Aerodynamic Characteristics Associated with a Series of Low-aspect-ration Wings Having Variations in Leading Contour written by Bernard Spencer and published by . This book was released on 1962 with total page 92 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Longitudinal Stability Characteristics of Low-aspect-ratio Wings Having Variations in Leading and Trailing-edge Contours

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ISBN 13 :
Total Pages : 56 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis Longitudinal Stability Characteristics of Low-aspect-ratio Wings Having Variations in Leading and Trailing-edge Contours by : William P. Henderson

Download or read book Longitudinal Stability Characteristics of Low-aspect-ratio Wings Having Variations in Leading and Trailing-edge Contours written by William P. Henderson and published by . This book was released on 1964 with total page 56 pages. Available in PDF, EPUB and Kindle. Book excerpt:

NASA Technical Note

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ISBN 13 :
Total Pages : 478 pages
Book Rating : 4.:/5 (319 download)

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Book Synopsis NASA Technical Note by :

Download or read book NASA Technical Note written by and published by . This book was released on 1970 with total page 478 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Aerodynamic Characteristics of Low-aspect-ratio Wings at High Supersonic Mach Numbers

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ISBN 13 :
Total Pages : 19 pages
Book Rating : 4.:/5 (11 download)

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Book Synopsis Aerodynamic Characteristics of Low-aspect-ratio Wings at High Supersonic Mach Numbers by : Edward F. Ulmann

Download or read book Aerodynamic Characteristics of Low-aspect-ratio Wings at High Supersonic Mach Numbers written by Edward F. Ulmann and published by . This book was released on 1953 with total page 19 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Effects of Wing Leading-edge Deflection on Low-speed Aerodynamic Characteristics of a Low-aspect-ratio Highly Swept Arrow-wing Configuration

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ISBN 13 :
Total Pages : 76 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis Effects of Wing Leading-edge Deflection on Low-speed Aerodynamic Characteristics of a Low-aspect-ratio Highly Swept Arrow-wing Configuration by : Paul L. Coe

Download or read book Effects of Wing Leading-edge Deflection on Low-speed Aerodynamic Characteristics of a Low-aspect-ratio Highly Swept Arrow-wing Configuration written by Paul L. Coe and published by . This book was released on 1979 with total page 76 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Effect of Aspect Ratio on the Low-speed Lateral Control Characteristics of Unswept Untapered Low-aspect-ratio Wings

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

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Book Synopsis Effect of Aspect Ratio on the Low-speed Lateral Control Characteristics of Unswept Untapered Low-aspect-ratio Wings by : Rodger L. Naeseth

Download or read book Effect of Aspect Ratio on the Low-speed Lateral Control Characteristics of Unswept Untapered Low-aspect-ratio Wings written by Rodger L. Naeseth and published by . This book was released on 1951 with total page 56 pages. Available in PDF, EPUB and Kindle. Book excerpt: A series of untapered, unswept, complete wings of apsect ratios 1.13, 2.13, 4.13, and 6.13 was investigated at a Mach number of 0.26 to determine the effect of aspect ratio on the lateral control characteristics of the wings equipped with 0.25-chord sealed ailerons of various spans and of various spanwise locations. Design charts are presented for computing aileron effectiveness of low-aspect-ratio, untapered, unswept wings. Experimental values of control effectivenesss are compared with values estimated by theoretical methods.

A Review of the Planform Effects on the Low-speed Aerodynamic Characteristics of Triangular and Modified Triangular Wings

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ISBN 13 :
Total Pages : 112 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis A Review of the Planform Effects on the Low-speed Aerodynamic Characteristics of Triangular and Modified Triangular Wings by : Kenneth Razak

Download or read book A Review of the Planform Effects on the Low-speed Aerodynamic Characteristics of Triangular and Modified Triangular Wings written by Kenneth Razak and published by . This book was released on 1966 with total page 112 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Wind-tunnel Investigation of Single and Tandem Low-aspect-ratio Wings in Ground Effect

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ISBN 13 :
Total Pages : 123 pages
Book Rating : 4.:/5 (86 download)

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Book Synopsis Wind-tunnel Investigation of Single and Tandem Low-aspect-ratio Wings in Ground Effect by : William D. Hinshaw

Download or read book Wind-tunnel Investigation of Single and Tandem Low-aspect-ratio Wings in Ground Effect written by William D. Hinshaw and published by . This book was released on 1964 with total page 123 pages. Available in PDF, EPUB and Kindle. Book excerpt: The effects of end-plate and camber changes on the aerodynamic characteristics of five basic wings in ground effect were investigated by the image technique, and the effect of gap-chord and aspect ratio was investigated on tandem-wing combinations over a ground board. For a given end-plate structural clearance height, the addition of end plates shows an increase in L/D for AR-1; however, better L/D is obtained with end plates off for AR-4. For a given wing trailing edge structural clearance height, end plates show considerable improvement in L/D. Improved L/D is also noted for (a) small down flap deflection, (b) contoured end plates, (c) wedge-bottom end plates, (d) thin wing, and (e) high aspect ratio. Static stability improves as the ground is approached and is particularly evident for the tandem-wing combinations. Limited data were obtained in roll and yaw. (Author).

NUREG/CR.

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ISBN 13 :
Total Pages : 108 pages
Book Rating : 4.:/5 (319 download)

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Book Synopsis NUREG/CR. by : U.S. Nuclear Regulatory Commission

Download or read book NUREG/CR. written by U.S. Nuclear Regulatory Commission and published by . This book was released on 1979 with total page 108 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Effects of Wing Leading-edge Deflection on Low-speed Aerodynamic Characteristics of a Low-aspect-ratio Highly Swept Arrow-wing Configuration

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ISBN 13 :
Total Pages : 76 pages
Book Rating : 4.:/5 (317 download)

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Book Synopsis Effects of Wing Leading-edge Deflection on Low-speed Aerodynamic Characteristics of a Low-aspect-ratio Highly Swept Arrow-wing Configuration by : P. L. Coe (Jr)

Download or read book Effects of Wing Leading-edge Deflection on Low-speed Aerodynamic Characteristics of a Low-aspect-ratio Highly Swept Arrow-wing Configuration written by P. L. Coe (Jr) and published by . This book was released on 1979 with total page 76 pages. Available in PDF, EPUB and Kindle. Book excerpt:

U.S. Government Research Reports

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ISBN 13 :
Total Pages : 1064 pages
Book Rating : 4.3/5 (243 download)

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Book Synopsis U.S. Government Research Reports by :

Download or read book U.S. Government Research Reports written by and published by . This book was released on 1961 with total page 1064 pages. Available in PDF, EPUB and Kindle. Book excerpt: