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A Transonic Wind Tunnel Investigation Of An Unswept Wing Body Combination At Angles Of Attack Up To 24 Degrees
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Book Synopsis A Transonic Wind-tunnel Investigation of an Unswept-wing-body Combination at Angles of Attack Up to 24 Degrees by : Bruce B. Estabrooks
Download or read book A Transonic Wind-tunnel Investigation of an Unswept-wing-body Combination at Angles of Attack Up to 24 Degrees written by Bruce B. Estabrooks and published by . This book was released on 1953 with total page 23 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Transonic Wind-tunnel Investigation of an Unswept Wing in Combination with a Systematic Series of Four Bodies by : Bruce B. Estabrooks
Download or read book Transonic Wind-tunnel Investigation of an Unswept Wing in Combination with a Systematic Series of Four Bodies written by Bruce B. Estabrooks and published by . This book was released on 1953 with total page 34 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Transonic Wind-tunnel Investigation of Aerodynamic-loading Characteristics of a 2-percent-thick Trapezoidal Wing in Combination with Basic and Indented Bodies by : Thomas C. Kelly
Download or read book Transonic Wind-tunnel Investigation of Aerodynamic-loading Characteristics of a 2-percent-thick Trapezoidal Wing in Combination with Basic and Indented Bodies written by Thomas C. Kelly and published by . This book was released on 1957 with total page 86 pages. Available in PDF, EPUB and Kindle. Book excerpt: Pressure data have been obtained in the Langley 8-foot transonic tunnel at Mach numbers from 0.80 to 1.115 and angles of attack from 0 to 20 degrees for wing-body configurations employing a thin trapezoidal wing in combination with basic and indented bodies. The wing had 26.6 degrees sweepback of the quarter-chord line, an aspect ratio of 2.61, a taper ratio of 0.211, and 2-percent-thick symmetrical circular-arc airfoil sections parallel to the plane of symmetry. Results are also presented for the basic body alone. Reynolds numbers for the tests were on the order of 2,600,000, based on the wing mean aerodynamic chord.
Book Synopsis Transonic Wind-tunnel Investigation of Static Longitudinal Force and Moment Characteristics of Two Wing-body Combinations with Clipped-tip and Full Delta Wings of Aspect Ratio 1.73 by : Dale L. Burrows
Download or read book Transonic Wind-tunnel Investigation of Static Longitudinal Force and Moment Characteristics of Two Wing-body Combinations with Clipped-tip and Full Delta Wings of Aspect Ratio 1.73 written by Dale L. Burrows and published by . This book was released on 1956 with total page 26 pages. Available in PDF, EPUB and Kindle. Book excerpt: An investigation has been made in the Langley transonic blowdown tunnel to obtain the static longitudinal force and moment characteristics of an aspect-ratio-1.73, 3-percent-thick delta wing and an aspect-ratio-1.73, 4-percent-thick clipped delta wing (taper ratio 4.0), each mounted on a slender body. Both wings had NACA 65A00X airfoil sections parallel to the body center line. The Mach number range was from 0.76 to 1.39 at angles of attack as high as 20 degrees. At low angles of attack, the Reynolds number was about 7,000,000 for the full delta and 6,000,000 for the clipped delta.
Book Synopsis A Transonic Wind-tunnel Investigation of the Effects of Body Indentation, as Specified by the Transonic Drag-rise Rule, on the Aerodynamic Characteristics and Flow Phenomena of an Unswept-wing-body Combination by : Claude V. Williams
Download or read book A Transonic Wind-tunnel Investigation of the Effects of Body Indentation, as Specified by the Transonic Drag-rise Rule, on the Aerodynamic Characteristics and Flow Phenomena of an Unswept-wing-body Combination written by Claude V. Williams and published by . This book was released on 1953 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis A Transonic Wind-tunnel Investigation of the Effects of Body Indention, as Specified by the Transonic Drag-rise Rule, on the Aerodynamic Characteristics and Flow Phenomena of an Unswept-wing-body Combination by : Claude V. Williams
Download or read book A Transonic Wind-tunnel Investigation of the Effects of Body Indention, as Specified by the Transonic Drag-rise Rule, on the Aerodynamic Characteristics and Flow Phenomena of an Unswept-wing-body Combination written by Claude V. Williams and published by . This book was released on 1953 with total page 38 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis A Transonic Wind-tunnel Investigation of the Effects of Body Indentation, as Specified by the Transonic Drag-rise Rule, on the Aerodynamic Characteristics and Flow Phenomena of a 45 Degree Sweptback-wing-body Combination by : Harold L. Robinson
Download or read book A Transonic Wind-tunnel Investigation of the Effects of Body Indentation, as Specified by the Transonic Drag-rise Rule, on the Aerodynamic Characteristics and Flow Phenomena of a 45 Degree Sweptback-wing-body Combination written by Harold L. Robinson and published by . This book was released on 1953 with total page 33 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 Transonic-wind Tunnel Investigation of the Effects of Wing Incidence Angle on the Characteristics of Two Wing-body Combinations by : Francis G. Jr Morgan
Download or read book Transonic-wind Tunnel Investigation of the Effects of Wing Incidence Angle on the Characteristics of Two Wing-body Combinations written by Francis G. Jr Morgan and published by . This book was released on 1953 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis A Transonic Wind-tunnel Investigation of the Effects of Body Indentation, as Specified by the Transonic Drag-rise Rule, on the Aerodynamic Characteristics and Flow Phenomena of a 45 Degrees Sweptback-wing-body Combination by : Harold L. Robinson
Download or read book A Transonic Wind-tunnel Investigation of the Effects of Body Indentation, as Specified by the Transonic Drag-rise Rule, on the Aerodynamic Characteristics and Flow Phenomena of a 45 Degrees Sweptback-wing-body Combination written by Harold L. Robinson and published by . This book was released on 1953 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
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 Transonic Wind-tunnel Investigation of the Aerodynamic Loading Characteristics of a Highly Tapered Upswept Wing in the Presence of a Body with and Without Indentation by : Joseph D. Brooks
Download or read book Transonic Wind-tunnel Investigation of the Aerodynamic Loading Characteristics of a Highly Tapered Upswept Wing in the Presence of a Body with and Without Indentation written by Joseph D. Brooks and published by . This book was released on 1956 with total page 30 pages. Available in PDF, EPUB and Kindle. Book excerpt: A transonic investigation of the aerodynamic loading characteristics and the effects of body indentation on the wing loads of a low-aspect-ratio, highly tapered, unswept wing in the presence of a body has been conducted in the Langley 8-foot transonic pressure tunnel. The tests covered a range of Mach numbers from 0.60 to 1.20 for angles of attack from 0 to 20 degrees.
Book Synopsis Transonic Wind-tunnel Investigation of the Aerodynamic Characteristics of a 60 Degree Triangular Wing in Combination with a Systematic Series of Three Bodies by : Thomas C. Kelly
Download or read book Transonic Wind-tunnel Investigation of the Aerodynamic Characteristics of a 60 Degree Triangular Wing in Combination with a Systematic Series of Three Bodies written by Thomas C. Kelly and published by . This book was released on 1953 with total page 22 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Scientific and Technical Aerospace Reports by :
Download or read book Scientific and Technical Aerospace Reports written by and published by . This book was released on 1989 with total page 1134 pages. Available in PDF, EPUB and Kindle. Book excerpt:
