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An Experimental Transonic Investigation Of A 45c Sweptback Wing Body Combination With Several Types Of Body Indentation With Theoretical Comparisons Included
Download An Experimental Transonic Investigation Of A 45c Sweptback Wing Body Combination With Several Types Of Body Indentation With Theoretical Comparisons Included full books in PDF, epub, and Kindle. Read online An Experimental Transonic Investigation Of A 45c Sweptback Wing Body Combination With Several Types Of Body Indentation With Theoretical Comparisons Included ebook anywhere anytime directly on your device. Fast Download speed and no annoying ads. We cannot guarantee that every ebooks is available!
Book Synopsis An Experimental Transonic Investigation of a 45 Degrees Sweptback Wing-body Combination with Several Types of Body Indentation with Theoretical Comparisons Included by : Melvin M. Carmel
Download or read book An Experimental Transonic Investigation of a 45 Degrees Sweptback Wing-body Combination with Several Types of Body Indentation with Theoretical Comparisons Included written by Melvin M. Carmel and published by . This book was released on 1954 with total page 51 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Transonic Wind-tunnel Investigation of the Effects of Incidence and Body Indentation on the Wing Loads of a 45 Degree Sweptback Wing-body Combination by : Robert J. Jr Platt
Download or read book Transonic Wind-tunnel Investigation of the Effects of Incidence and Body Indentation on the Wing Loads of a 45 Degree Sweptback Wing-body Combination written by Robert J. Jr Platt and published by . This book was released on 1956 with total page 24 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Influence of the Body Flow Field on the Zero-lift Wave Drag of Wing-body Combinations Modified in Accordance with the Transonic Area Rule by : William A. Page
Download or read book Influence of the Body Flow Field on the Zero-lift Wave Drag of Wing-body Combinations Modified in Accordance with the Transonic Area Rule written by William A. Page and published by . This book was released on 1956 with total page 32 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Transonic Aerodynamic Loading Characteristics of a Wing-body-tail Combination Having 52.5° Sweptback Wing of Aspect Ratio 3 with Conical Wing Camber and Body Indentation for a Design Mach Number [square Root Of] 2 by : Marlowe D. Cassetti
Download or read book Transonic Aerodynamic Loading Characteristics of a Wing-body-tail Combination Having 52.5° Sweptback Wing of Aspect Ratio 3 with Conical Wing Camber and Body Indentation for a Design Mach Number [square Root Of] 2 written by Marlowe D. Cassetti and published by . This book was released on 1961 with total page 104 pages. Available in PDF, EPUB and Kindle. Book excerpt: An investigation has been made of the effects of conical wing camber and body indentation according to the supersonic area rule on the aerodynamic wing loading characteristics of a wing-body-tail configuration at transonic speeds. The wing aspect ratio was 3, taper ratio was 0.1, and quarter-chord-line sweepback was 52.5° with 3-percent-thick airfoil sections. The tests were conducted in the Langley 16-foot transonic tunnel at Mach numbers from 0.80 to 1.05 and at angles of attack from 0° to 14°, with Reynolds numbers based on mean aerodynamic chord varying from 7 x 106 to 8 x 106. Conical camber delayed wing-tip stall and reduced the severity of the accompanying longitudinal instability but did not appreciably affect the spanwise load distribution at angles of attack below tip stall. Body indentation reduced to transonic chordwise center-of-pressure travel from about 8 percent to 5 percent of the mean aerodynamic chord.
Book Synopsis Investigation of the Effect of Indentation on an M-plan-form-wing--body Combination at Transonic Speeds by : Donald L. Loving
Download or read book Investigation of the Effect of Indentation on an M-plan-form-wing--body Combination at Transonic Speeds written by Donald L. Loving and published by . This book was released on 1954 with total page 24 pages. Available in PDF, EPUB and Kindle. Book excerpt: The effect of body indentation on the aerodynamic characteristics of an M-plan-form-wing-body combination has been investigated for angles of attack 0 to 12 percent at Mach numbers from 0.80 to 1.13 in the Langley 8-foot transonic tunnel. The Reynolds number of the investigation varied from 1,600,000 to 1,660,000. The M-wing with 45 degrees sweep angles was tested on a plain body and a body with an indentation that was 65 percent of that required for a Mach number of 1.0. A similar 45 degree sweptback wing was tested on a plain body to furnish basic comparison information.
Book Synopsis A Transonic Wind-tunnel Investigation of the Effect of Modifications to an Indented Body in Combination with a 45 Degree Sweptback Wing by : Donald L. Loving
Download or read book A Transonic Wind-tunnel Investigation of the Effect of Modifications to an Indented Body in Combination with a 45 Degree Sweptback Wing written by Donald L. Loving and published by . This book was released on 1953 with total page 29 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Transonic Wind-tunnel Investigation of the Effects of Body Indentation for Boattail and Cylindrical Afterbody Shapes on the Aerodynamic Characteristics of an Unswept-wing - Body Combination by : Thomas C. Kelly
Download or read book Transonic Wind-tunnel Investigation of the Effects of Body Indentation for Boattail and Cylindrical Afterbody Shapes on the Aerodynamic Characteristics of an Unswept-wing - Body Combination written by Thomas C. Kelly and published by . This book was released on 1954 with total page 22 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis A Transonic Wind-tunnel Investigation of the Effects of Twist and Camber with and Without Incidence, Twist, and Body Indentation on the Aerodynamic Characteristics of a 45 Degree Sweptback Wing-body Configuration by : J. Lawrence Cooper
Download or read book A Transonic Wind-tunnel Investigation of the Effects of Twist and Camber with and Without Incidence, Twist, and Body Indentation on the Aerodynamic Characteristics of a 45 Degree Sweptback Wing-body Configuration written by J. Lawrence Cooper and published by . This book was released on 1954 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Subsonic Investigation of Effects of Body Indentation on Zero-lift Drag Characteristics of a 45 Degree Sweptback Wing-body Combination with Natural and Fixed Boundary-layer Transition Through a Range of Reynolds Number 1 X (10)6 to 8 X (10)6 by : Gene J. Bingham
Download or read book Subsonic Investigation of Effects of Body Indentation on Zero-lift Drag Characteristics of a 45 Degree Sweptback Wing-body Combination with Natural and Fixed Boundary-layer Transition Through a Range of Reynolds Number 1 X (10)6 to 8 X (10)6 written by Gene J. Bingham and published by . This book was released on 1954 with total page 10 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis An Investigation of Wing-body Juncture Interference Effects at Transonic Speeds for Several Swept-wing and Body Combinations by : John B. McDevitt
Download or read book An Investigation of Wing-body Juncture Interference Effects at Transonic Speeds for Several Swept-wing and Body Combinations written by John B. McDevitt and published by . This book was released on 1957 with total page 107 pages. Available in PDF, EPUB and Kindle. Book excerpt: This report presents the results of an investigation of wing-body juncture interference effects at high subsonic and transonic speeds. Force characteristics and pressure measurements for various bodies in combination with sweptback wings of aspect ratios 3 and 6 were obtained through a Mach number range from 0.8 to 1.2. The bodies used consisted of basic Sears-Haack bodies of revolution, the basic bodies indented by area-rule concepts at design Mach numbers of 1.0 and 1.2, and the latter area-rule bodies reshaped without-change in cross-sectional areas (by the superposition of slender-body multiples) so that the flow along the wing-body juncture chords at high subsonic speeds more closely resembled that for the infinite oblique wing.
Book Synopsis The Effect of a Change in Body Shape on the Loading of a 45 Degree Sweptback Wing-body Combination at Transonic Speeds by : Donald L. Loving
Download or read book The Effect of a Change in Body Shape on the Loading of a 45 Degree Sweptback Wing-body Combination at Transonic Speeds written by Donald L. Loving and published by . This book was released on 1954 with total page 67 pages. Available in PDF, EPUB and Kindle. Book excerpt: An investigation was made in the Langley 8-foot transonic tunnel of the pressure distribution on a wing-body combination having a 45 degree swept-back wing with aspect ratio 4, taper ratio 0.6, and NACA 65A006 airfoil sections parallel to the plane of symmetry. The body had an afterbody which was cylindrical from the region of the leading edge of the wing-body juncture rearward to the base. Data were obtained at Mach number from 0.60 to 1.13. The test Reynolds numbers ranged from 1,740,000 to 2,030,000. In order to determine the effects on loads of a change in body shape, the results of this investigation are compared with similar data previously obtained for the same wing in combination with a body that was curved from the nose to the base.
Book Synopsis Transonic Aerodynamic Characteristics of a Wing-body Combination Having a 52.20 Sweptback Wing of Aspect Ratio 3 with Conical Camber and Designed for a Mach Number of 2 by : William B. Igoe
Download or read book Transonic Aerodynamic Characteristics of a Wing-body Combination Having a 52.20 Sweptback Wing of Aspect Ratio 3 with Conical Camber and Designed for a Mach Number of 2 written by William B. Igoe and published by . This book was released on 1961 with total page 56 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Transonic Aerodynamic Characteristics of a Wing-Body Combination Having a 52.5 Deg Sweptback Wing of Aspect Ratio 3 with Conical Camber and Designed for a Mach Number of the Square Root of 2 by : William B. Igoe
Download or read book Transonic Aerodynamic Characteristics of a Wing-Body Combination Having a 52.5 Deg Sweptback Wing of Aspect Ratio 3 with Conical Camber and Designed for a Mach Number of the Square Root of 2 written by William B. Igoe and published by . This book was released on 1961 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis An Experimental Investigation at a Mach Number of 2.01 of the Effects of Body Cross-section Shape on the Aerodynamic Characteristics of Bodies and Wing-body Combinations by : Harry W. Carlson
Download or read book An Experimental Investigation at a Mach Number of 2.01 of the Effects of Body Cross-section Shape on the Aerodynamic Characteristics of Bodies and Wing-body Combinations written by Harry W. Carlson and published by . This book was released on 1955 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt: Abstract: An experimental investigation has been performed to determine the effect of changes in body cross-section shape on the aerodynamic characteristics of bodies and wing-body combinations. A series of 13 bodies having a given length and given longitudinal distribution of cross-sectional area but various cross-section shapes were tested at a Mach number of 2.01. The bodies were tested alone and in combination with a 47° sweptback wing having a 6-percent-thick hexagonal section.
Book Synopsis An Investigation of the Transonic Area Rule by Flight Tests of a Sweptback Wing on a Cylindrical Body with and Without Body Indentation Between Mach Numbers 0.9 and 1.8 by : Sherwood Hoffman
Download or read book An Investigation of the Transonic Area Rule by Flight Tests of a Sweptback Wing on a Cylindrical Body with and Without Body Indentation Between Mach Numbers 0.9 and 1.8 written by Sherwood Hoffman and published by . This book was released on 1953 with total page 24 pages. Available in PDF, EPUB and Kindle. Book excerpt:
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