Aerodynamic Loads On An External Store Adjacent To A 45 Degree Sweptback Wing At Mach Numbers From 070 To 196 Including An Evaluation Of Techniques Used

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Aerodynamic Loads on an External Store Adjacent to a 45 Degree Sweptback Wing at Mach Numbers from 0.70 to 1.96, Including an Evaluation of Techniques Used

Author : Lawrence D. Guy
Publisher :
ISBN 13 :
Total Pages : 109 pages
Book Rating : 4.:/5 (721 download)

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Book Synopsis Aerodynamic Loads on an External Store Adjacent to a 45 Degree Sweptback Wing at Mach Numbers from 0.70 to 1.96, Including an Evaluation of Techniques Used by : Lawrence D. Guy

Download or read book Aerodynamic Loads on an External Store Adjacent to a 45 Degree Sweptback Wing at Mach Numbers from 0.70 to 1.96, Including an Evaluation of Techniques Used written by Lawrence D. Guy and published by . This book was released on 1955 with total page 109 pages. Available in PDF, EPUB and Kindle. Book excerpt: Aerodynamic forces and moments have been obtained in the Langley 9- by 12-inch blowdown tunnel on an external store and on a 45 degree swept-back wing-body combination measured separately at Mach numbers from 0.70 to 1.96. The wing was cantilevered and had an aspect ratio of 4.0; the store was independently sting-mounted and had a Douglas Aircraft Co. (DAC) store shape. The angle of attack range was from -3 degrees to 12 degrees and the Reynolds number (based on wing mean aerodynamic chord) varied from 1.2 x10(6) to 1.7 x 10(6). Wing-body transonic forces and moments have been compared with data of a geometrically similar full-scale model tested in the Langley 16-foot and 8-foot transonic tunnels in order to aid in the evaluation of transonic-tunnel interference.

Aerodynamic Loads on an External Store Adjacent to a 45° Sweptback Wing at Mach Numbers from 0.70 to 1.96, Including an Evaluation of Techniques Used

Download Aerodynamic Loads on an External Store Adjacent to a 45° Sweptback Wing at Mach Numbers from 0.70 to 1.96, Including an Evaluation of Techniques Used PDF Online Free

Author : Lawrence Duncan Guy
Publisher :
ISBN 13 :
Total Pages : 109 pages
Book Rating : 4.:/5 (71 download)

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Book Synopsis Aerodynamic Loads on an External Store Adjacent to a 45° Sweptback Wing at Mach Numbers from 0.70 to 1.96, Including an Evaluation of Techniques Used by : Lawrence Duncan Guy

Download or read book Aerodynamic Loads on an External Store Adjacent to a 45° Sweptback Wing at Mach Numbers from 0.70 to 1.96, Including an Evaluation of Techniques Used written by Lawrence Duncan Guy and published by . This book was released on 1955 with total page 109 pages. Available in PDF, EPUB and Kindle. Book excerpt: Aerodynamic forces and moments have been obtained in the Langley 9- by 12-inch blowdown tunnel on an external store and on a 45° sweptback wing-body combination measured separately at Mach numbers from 0.70 to 1.96. The wing was cantilevered and had an aspect ratio of 4.0; the store was independently sting-mounted and had a Douglas Aircraft Co. (DAC) store shape. The angle-of-attack range was from -3° to 12° and the Reynolds number (based on wing mean aerodynamic chord) varied from 1.2 x 106 to 1.7 x 106. Wing-body transonic forces and moments have been compared with data of a geometrically similar full-scale model tested in the Langley 16-foot and 8-foot transonic tunnels in order to aid in the evaluation of transonic-tunnel interference.

Some Notes on the Aerodynamic Loads Associated with External-store Installations

Author : H. Norman Silvers
Publisher :
ISBN 13 :
Total Pages : 22 pages
Book Rating : 4.3/5 (91 download)

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Book Synopsis Some Notes on the Aerodynamic Loads Associated with External-store Installations by : H. Norman Silvers

Download or read book Some Notes on the Aerodynamic Loads Associated with External-store Installations written by H. Norman Silvers and published by . This book was released on 1953 with total page 22 pages. Available in PDF, EPUB and Kindle. Book excerpt: The results presented in this paper indicate that the effects of stores on wing load distribution at subsonic speeds may be predicted by available methods at the lower angles of attack where wing flow separation is negligible. At the higher angles of attack where wing flow separation exists, a store located inboard on a swept wing may act much like various devices designed to delay wing pitch-up by reducing the loss in load at the wing tip due to flow separation. Furthermore, the results indicate that the normal force and pitching moment of a store located at the wing tip can be calculated quite well by available methods. On the other hand, no theoretical procedure is available to calculate the severe lateral forces and moments encountered at zero sideslip on an inboard arrangement of stores on a swept wing.

Aerodynamic Loads on an External Store Adjacent to an Unswept Wing at Mach Numbers Between 0.75 and 1.96

Author : William M. Hadaway
Publisher :
ISBN 13 :
Total Pages : 61 pages
Book Rating : 4.:/5 (696 download)

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Book Synopsis Aerodynamic Loads on an External Store Adjacent to an Unswept Wing at Mach Numbers Between 0.75 and 1.96 by : William M. Hadaway

Download or read book Aerodynamic Loads on an External Store Adjacent to an Unswept Wing at Mach Numbers Between 0.75 and 1.96 written by William M. Hadaway and published by . This book was released on 1956 with total page 61 pages. Available in PDF, EPUB and Kindle. Book excerpt: An investigation of the aerodynamic forces and moments on both an unswept wing and a sting-mounted store at various locations below the wing has been made in the Langley 9- by 12-inch blowdown tunnel at Mach numbers from 0.75 to 1.96. The semispan wing had an aspect ratio of 4.0, a taper ratio of 0.6, and NACA 65A004 airfoil sections. The store had a Douglas Aircraft Company shape and was sting mounted independently of the cantilevered semispan sting-mounted wing-body combination. Forces and moments on the store and on the wing-body were measured simultaneously through an angle-of-attack range of -3° to 12°.

Aerodynamic Loading Characteristics in Sideslip of a 45© Sweptback Wing with and Without a Fence at High Subsonic Speeds

Author : Richard E. Kuhn
Publisher :
ISBN 13 :
Total Pages : 50 pages
Book Rating : 4.3/5 (91 download)

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Book Synopsis Aerodynamic Loading Characteristics in Sideslip of a 45© Sweptback Wing with and Without a Fence at High Subsonic Speeds by : Richard E. Kuhn

Download or read book Aerodynamic Loading Characteristics in Sideslip of a 45© Sweptback Wing with and Without a Fence at High Subsonic Speeds written by Richard E. Kuhn and published by . This book was released on 1955 with total page 50 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Effects of Size of External Stores on the Aerodynamic Characteristics of an Unswept and a 45 Degree Sweptback Wing of Aspect Ratio 4 and a 60 Degree Delta Wing at Mach Numbers of 1.41, 1.62, and 1.96

Download Effects of Size of External Stores on the Aerodynamic Characteristics of an Unswept and a 45 Degree Sweptback Wing of Aspect Ratio 4 and a 60 Degree Delta Wing at Mach Numbers of 1.41, 1.62, and 1.96 PDF Online Free

Author : Carl R. Jacobsen
Publisher :
ISBN 13 :
Total Pages : 55 pages
Book Rating : 4.:/5 (11 download)

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Book Synopsis Effects of Size of External Stores on the Aerodynamic Characteristics of an Unswept and a 45 Degree Sweptback Wing of Aspect Ratio 4 and a 60 Degree Delta Wing at Mach Numbers of 1.41, 1.62, and 1.96 by : Carl R. Jacobsen

Download or read book Effects of Size of External Stores on the Aerodynamic Characteristics of an Unswept and a 45 Degree Sweptback Wing of Aspect Ratio 4 and a 60 Degree Delta Wing at Mach Numbers of 1.41, 1.62, and 1.96 written by Carl R. Jacobsen and published by . This book was released on 1953 with total page 55 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Introduction to Aircraft Flight Mechanics

Author : Thomas R. Yechout
Publisher : AIAA
ISBN 13 : 9781600860782
Total Pages : 666 pages
Book Rating : 4.8/5 (67 download)

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Book Synopsis Introduction to Aircraft Flight Mechanics by : Thomas R. Yechout

Download or read book Introduction to Aircraft Flight Mechanics written by Thomas R. Yechout and published by AIAA. This book was released on 2003 with total page 666 pages. Available in PDF, EPUB and Kindle. Book excerpt: Based on a 15-year successful approach to teaching aircraft flight mechanics at the US Air Force Academy, this text explains the concepts and derivations of equations for aircraft flight mechanics. It covers aircraft performance, static stability, aircraft dynamics stability and feedback control.

Aerodynamic Loads on Four External Stores in the Carriage Position on the A-7D and F-4C Aircraft at Mach Numbers from 0.5 to 2.0

Author : David W Hill (Jr)
Publisher :
ISBN 13 :
Total Pages : 54 pages
Book Rating : 4.:/5 (227 download)

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Book Synopsis Aerodynamic Loads on Four External Stores in the Carriage Position on the A-7D and F-4C Aircraft at Mach Numbers from 0.5 to 2.0 by : David W Hill (Jr)

Download or read book Aerodynamic Loads on Four External Stores in the Carriage Position on the A-7D and F-4C Aircraft at Mach Numbers from 0.5 to 2.0 written by David W Hill (Jr) and published by . This book was released on 1974 with total page 54 pages. Available in PDF, EPUB and Kindle. Book excerpt: Aerodynamic force and moment measurements were made on 0.05-scale models of the M-117GP and BLU-1C/B bombs, the 300-gal fuel tank, and the AGM-62/A Walleye missile in the carriage position on the A-7D and F-4C aircraft at Mach numbers from 0.5 to 2.0. The aircraft model angle of attack was varied from -4 to 12 deg and the yaw angle from -8 to 8 deg. Studies were made to evaluate the effects of store nose shape variation and store location on the multiple ejection rack and pylon on the measured aerodynamic coefficients. This report contains a description of the test along with information to identify test configurations and test conditions for all data obtained. Only a limited amount of data is presented to show the magnitude of the store aerodynamic loads and variations caused by changes in the aircraft configuration. (Author).

Effects of the Spanwise, Chordwise, and Vertical Location of an External Store on the Aerodynamic Characteristics of a 45 Degree Sweptback Tapered Wing of Aspect Ratio 4 at Mach Numbers of 1.41, 1.62, and 1.96

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Author : Carl R. Jacobsen
Publisher :
ISBN 13 :
Total Pages : 31 pages
Book Rating : 4.:/5 (11 download)

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Book Synopsis Effects of the Spanwise, Chordwise, and Vertical Location of an External Store on the Aerodynamic Characteristics of a 45 Degree Sweptback Tapered Wing of Aspect Ratio 4 at Mach Numbers of 1.41, 1.62, and 1.96 by : Carl R. Jacobsen

Download or read book Effects of the Spanwise, Chordwise, and Vertical Location of an External Store on the Aerodynamic Characteristics of a 45 Degree Sweptback Tapered Wing of Aspect Ratio 4 at Mach Numbers of 1.41, 1.62, and 1.96 written by Carl R. Jacobsen and published by . This book was released on 1953 with total page 31 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Investigation at Transonic Speeds of the Loading Over a 45 Degree Sweptback Wing Having an Aspect Ratio of 3, a Taper Ratio of 0.2, and Naca 65a004 Airfoil Sections

Download Investigation at Transonic Speeds of the Loading Over a 45 Degree Sweptback Wing Having an Aspect Ratio of 3, a Taper Ratio of 0.2, and Naca 65a004 Airfoil Sections PDF Online Free

Author : JACK F. RUNCKEL
Publisher :
ISBN 13 :
Total Pages : 1 pages
Book Rating : 4.:/5 (227 download)

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Book Synopsis Investigation at Transonic Speeds of the Loading Over a 45 Degree Sweptback Wing Having an Aspect Ratio of 3, a Taper Ratio of 0.2, and Naca 65a004 Airfoil Sections by : JACK F. RUNCKEL

Download or read book Investigation at Transonic Speeds of the Loading Over a 45 Degree Sweptback Wing Having an Aspect Ratio of 3, a Taper Ratio of 0.2, and Naca 65a004 Airfoil Sections written by JACK F. RUNCKEL and published by . This book was released on 1961 with total page 1 pages. Available in PDF, EPUB and Kindle. Book excerpt: An investigation at transonic speeds of the loading over a 45 degree sweptback wing having an aspect ratio of 3, a taper ratio of 0.2, and NACA 65A004 airfoil sections was conducted in the Langley 16-foot transonic tunnel. Pressure measurements on the wing-body combi ation were obtained at angles of attack from 0 degrees to 26 degrees at Mach numbers from 0.80 to 0.98 and at angles of attack from 0 degrees to about 12 degrees at Mach numbers from 1.00 to 1.05. Reynolds number, based on the wing mean aerodynamic c ord varied from 7 times 10 to the 6th po er to 8.5 times 10 to the 6th power over the test Mach number range. Results of the investigation indicate that a highly swept shock originates at the juncture of the wing leading edge and the body at moderate angles of attack and has a large influence on the loading over the inboard wing sections. (Author).

Effects of External Store Pylon Configuration and Position on the Aerodynamic Characteristics of a 45 Degree Swept Wing-fuselage Combination at a Mach Number of 1.61

Download Effects of External Store Pylon Configuration and Position on the Aerodynamic Characteristics of a 45 Degree Swept Wing-fuselage Combination at a Mach Number of 1.61 PDF Online Free

Author : Odell A. Morris
Publisher :
ISBN 13 :
Total Pages : 52 pages
Book Rating : 4.:/5 (11 download)

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Book Synopsis Effects of External Store Pylon Configuration and Position on the Aerodynamic Characteristics of a 45 Degree Swept Wing-fuselage Combination at a Mach Number of 1.61 by : Odell A. Morris

Download or read book Effects of External Store Pylon Configuration and Position on the Aerodynamic Characteristics of a 45 Degree Swept Wing-fuselage Combination at a Mach Number of 1.61 written by Odell A. Morris and published by . This book was released on 1958 with total page 52 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Aerodynamic Load Distribution Over a 45 Degree Swept Wing Having a Spoiler-slot-deflector Aileron and Other Spoiler Ailerons for Mach Numbers from 0.60 to 1.03

Download Aerodynamic Load Distribution Over a 45 Degree Swept Wing Having a Spoiler-slot-deflector Aileron and Other Spoiler Ailerons for Mach Numbers from 0.60 to 1.03 PDF Online Free

Author : F.E. Jr West
Publisher :
ISBN 13 :
Total Pages : 118 pages
Book Rating : 4.:/5 (11 download)

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Book Synopsis Aerodynamic Load Distribution Over a 45 Degree Swept Wing Having a Spoiler-slot-deflector Aileron and Other Spoiler Ailerons for Mach Numbers from 0.60 to 1.03 by : F.E. Jr West

Download or read book Aerodynamic Load Distribution Over a 45 Degree Swept Wing Having a Spoiler-slot-deflector Aileron and Other Spoiler Ailerons for Mach Numbers from 0.60 to 1.03 written by F.E. Jr West and published by . This book was released on 1957 with total page 118 pages. Available in PDF, EPUB and Kindle. Book excerpt:

The Effects of an Inverse-taper Leading-edge Flap on the Aerodynamic Loading of a 45 Degree Sweptback Wing at Mach Numbers to 0.90

Author : Fred A. Demele
Publisher :
ISBN 13 :
Total Pages : 108 pages
Book Rating : 4.:/5 (621 download)

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Book Synopsis The Effects of an Inverse-taper Leading-edge Flap on the Aerodynamic Loading of a 45 Degree Sweptback Wing at Mach Numbers to 0.90 by : Fred A. Demele

Download or read book The Effects of an Inverse-taper Leading-edge Flap on the Aerodynamic Loading of a 45 Degree Sweptback Wing at Mach Numbers to 0.90 written by Fred A. Demele and published by . This book was released on 1959 with total page 108 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Fundamentals of Flight

Author : Richard Shepherd Shevell
Publisher : Pearson Education India
ISBN 13 : 9788177587425
Total Pages : 468 pages
Book Rating : 4.5/5 (874 download)

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Book Synopsis Fundamentals of Flight by : Richard Shepherd Shevell

Download or read book Fundamentals of Flight written by Richard Shepherd Shevell and published by Pearson Education India. This book was released on 1989 with total page 468 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Aerodynamics of Wings and Bodies

Author : Holt Ashley
Publisher : Courier Corporation
ISBN 13 : 0486648990
Total Pages : 306 pages
Book Rating : 4.4/5 (866 download)

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Book Synopsis Aerodynamics of Wings and Bodies by : Holt Ashley

Download or read book Aerodynamics of Wings and Bodies written by Holt Ashley and published by Courier Corporation. This book was released on 1965-01-01 with total page 306 pages. Available in PDF, EPUB and Kindle. Book excerpt: This excellent, innovative reference offers a wealth of useful information and a solid background in the fundamentals of aerodynamics. Fluid mechanics, constant density inviscid flow, singular perturbation problems, viscosity, thin-wing and slender body theories, drag minimalization, and other essentials are addressed in a lively, literate manner and accompanied by diagrams.

Beyond Tube-and-Wing

Author : Bruce Larrimer
Publisher :
ISBN 13 : 9781626830592
Total Pages : pages
Book Rating : 4.8/5 (35 download)

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Book Synopsis Beyond Tube-and-Wing by : Bruce Larrimer

Download or read book Beyond Tube-and-Wing written by Bruce Larrimer and published by . This book was released on 2020-06-15 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:

Low-Speed Wind Tunnel Testing

Author : Jewel B. Barlow
Publisher : John Wiley & Sons
ISBN 13 : 0471557749
Total Pages : 738 pages
Book Rating : 4.4/5 (715 download)

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Book Synopsis Low-Speed Wind Tunnel Testing by : Jewel B. Barlow

Download or read book Low-Speed Wind Tunnel Testing written by Jewel B. Barlow and published by John Wiley & Sons. This book was released on 1999-02-22 with total page 738 pages. Available in PDF, EPUB and Kindle. Book excerpt: A brand-new edition of the classic guide on low-speed wind tunnel testing While great advances in theoretical and computational methods have been made in recent years, low-speed wind tunnel testing remains essential for obtaining the full range of data needed to guide detailed design decisions for many practical engineering problems. This long-awaited Third Edition of William H. Rae, Jr.'s landmark reference brings together essential information on all aspects of low-speed wind tunnel design, analysis, testing, and instrumentation in one easy-to-use resource. Written by authors who are among the most respected wind tunnel engineers in the world, this edition has been updated to address current topics and applications, and includes coverage of digital electronics, new instrumentation, video and photographic methods, pressure-sensitive paint, and liquid crystal-based measurement methods. The book is organized for quick access to topics of interest, and examines basic test techniques and objectives of modeling and testing aircraft designs in low-speed wind tunnels, as well as applications to fluid motion analysis, automobiles, marine vessels, buildings, bridges, and other structures subject to wind loading. Supplemented with real-world examples throughout, Low-Speed Wind Tunnel Testing, Third Edition is an indispensable resource for aerospace engineering students and professionals, engineers and researchers in the automotive industries, wind tunnel designers, architects, and others who need to get the most from low-speed wind tunnel technology and experiments in their work.