Gust-tunnel Investigation of a Wing Model with Semichord Line Swept Back 60 Degrees

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ISBN 13 :
Total Pages : 688 pages
Book Rating : 4.F/5 ( download)

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Book Synopsis Gust-tunnel Investigation of a Wing Model with Semichord Line Swept Back 60 Degrees by : Harold B. Pierce

Download or read book Gust-tunnel Investigation of a Wing Model with Semichord Line Swept Back 60 Degrees written by Harold B. Pierce and published by . This book was released on 1950 with total page 688 pages. Available in PDF, EPUB and Kindle. Book excerpt: An investigation was made in the Langley gust tunnel of a 60 degree sweptback-wing model to determine its response to gusts. On the basis of results, a simplified method of analysis, which uses a slope of the lift curve derived by the cosine law and which uses strip theory to estimate the penetration effect, appears to be applicable for the prediction of gust loads on wings swept as much as 60 degrees.

Gust-tunnel Investigation of a Flexible-wing Model with Semichord Line Swept Back 45°

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Publisher :
ISBN 13 :
Total Pages : 20 pages
Book Rating : 4.3/5 (91 download)

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Book Synopsis Gust-tunnel Investigation of a Flexible-wing Model with Semichord Line Swept Back 45° by : Thomas D. Reisert

Download or read book Gust-tunnel Investigation of a Flexible-wing Model with Semichord Line Swept Back 45° written by Thomas D. Reisert and published by . This book was released on 1949 with total page 20 pages. Available in PDF, EPUB and Kindle. Book excerpt: An investigation was made in the Langley gust tunnel of a flexible-wing model with the semichord line swept back 45 degrees to obtain experimental data on the amount of gust-load alleviation that might be expected as a result of the wings flexing under load. The results indicated that unless adverse pitching motion could be eliminated or reduced the over-all load reduction would be small. The net reduction in bending moment, however, may be appreciable.

Effect of Structural Flexibiligy on Aircraft Loading

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ISBN 13 :
Total Pages : 108 pages
Book Rating : 4.3/5 (91 download)

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Book Synopsis Effect of Structural Flexibiligy on Aircraft Loading by : Franklin O. Carta

Download or read book Effect of Structural Flexibiligy on Aircraft Loading written by Franklin O. Carta and published by . This book was released on 1953 with total page 108 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Proceedings of the ... U.S. National Congress of Applied Mechanics

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ISBN 13 :
Total Pages : 858 pages
Book Rating : 4.3/5 (97 download)

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Book Synopsis Proceedings of the ... U.S. National Congress of Applied Mechanics by :

Download or read book Proceedings of the ... U.S. National Congress of Applied Mechanics written by and published by . This book was released on 1954 with total page 858 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Wind-tunnel Investigation of Effect of Sweep on Rolling Derivatives at Angles of Attack Up to 13© and at High Subsonic Mach Numbers, Including a Semiempirical Method of Estimating the Rolling Derivatives

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ISBN 13 :
Total Pages : 54 pages
Book Rating : 4.3/5 (91 download)

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Book Synopsis Wind-tunnel Investigation of Effect of Sweep on Rolling Derivatives at Angles of Attack Up to 13© and at High Subsonic Mach Numbers, Including a Semiempirical Method of Estimating the Rolling Derivatives by : James W. Wiggins

Download or read book Wind-tunnel Investigation of Effect of Sweep on Rolling Derivatives at Angles of Attack Up to 13© and at High Subsonic Mach Numbers, Including a Semiempirical Method of Estimating the Rolling Derivatives written by James W. Wiggins and published by . This book was released on 1954 with total page 54 pages. Available in PDF, EPUB and Kindle. Book excerpt: An investigation was performed in the Langley high-speed 7- by 10-foot tunnel in order to determine the rolling derivatives for swept-wing-body configurations at angles of attack from 0 degrees to 13 degrees and at high subsonic Mach numbers. The wings had sweep angles of 3.6 degrees, 32.6 degrees, 45 degrees, and 60 degrees at the quarter-chord line, an aspect ratio of 4, a taper ratio of 0.6, and an NACA 65A006 airfoil section parallel to the free stream. The results indicate a reduction in the damping-in-roll derivative at the higher test angles of attack. Of the wings tested, instability of the damping-in-roll derivative was experienced over the largest ranges of angle of attack and Mach number for the 32.6 sweptback wing.

Aeronautical Engineering Review

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Publisher :
ISBN 13 :
Total Pages : 1456 pages
Book Rating : 4.3/5 (91 download)

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Book Synopsis Aeronautical Engineering Review by :

Download or read book Aeronautical Engineering Review written by and published by . This book was released on 1951 with total page 1456 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Aeronautical Engineering Index

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Publisher :
ISBN 13 :
Total Pages : 226 pages
Book Rating : 4.:/5 (319 download)

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Book Synopsis Aeronautical Engineering Index by :

Download or read book Aeronautical Engineering Index written by and published by . This book was released on 1952 with total page 226 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Aerospace Engineering Index

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ISBN 13 :
Total Pages : 788 pages
Book Rating : 4.3/5 (91 download)

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Book Synopsis Aerospace Engineering Index by :

Download or read book Aerospace Engineering Index written by and published by . This book was released on 1950 with total page 788 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Low-speed Wind-tunnel Investigation of a Triangular Sweptback Air Inlet in the Root of a 45 Degree Sweptback Wing

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ISBN 13 :
Total Pages : 76 pages
Book Rating : 4.3/5 (91 download)

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Book Synopsis Low-speed Wind-tunnel Investigation of a Triangular Sweptback Air Inlet in the Root of a 45 Degree Sweptback Wing by : Arvid L. Keith

Download or read book Low-speed Wind-tunnel Investigation of a Triangular Sweptback Air Inlet in the Root of a 45 Degree Sweptback Wing written by Arvid L. Keith and published by . This book was released on 1950 with total page 76 pages. Available in PDF, EPUB and Kindle. Book excerpt: A low-speed investigation has been conducted in the Langley two-dimensional low-turbulence tunnel to study a sweptback wing-root air-inlet configuration believed suitable for transonic-speed jet-powered airplanes. The test configurations consisted of a basic model with an NACA 64-008 wing with quarter-chord sweepback of 45 degrees mounted in the midwing position on a fuselage of fineness ratio 6.7, and an inlet model which had a triangular-shaped sweptback inlet installed in the wing root.

Aeroacoustics of Flight Vehicles

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ISBN 13 :
Total Pages : 620 pages
Book Rating : 4.F/5 ( download)

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Book Synopsis Aeroacoustics of Flight Vehicles by : Harvey H. Hubbard

Download or read book Aeroacoustics of Flight Vehicles written by Harvey H. Hubbard and published by . This book was released on 1991 with total page 620 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Aerodynamics of V/STOL Flight

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Publisher : Courier Corporation
ISBN 13 : 9780486404608
Total Pages : 356 pages
Book Rating : 4.4/5 (46 download)

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Book Synopsis Aerodynamics of V/STOL Flight by : Barnes Warnock McCormick

Download or read book Aerodynamics of V/STOL Flight written by Barnes Warnock McCormick and published by Courier Corporation. This book was released on 1999-01-01 with total page 356 pages. Available in PDF, EPUB and Kindle. Book excerpt: An extremely practical overview of V/STOL (vertical/short takeoff and landing) aerodynamics, this volume offers a presentation of general theoretical and applied aerodynamic principles, covering propeller and helicopter rotor theory for both the static and forward flight cases. Both a text for students and a reference for professionals, the book can be used for advanced undergraduate or graduate courses. Numerous detailed figures, plus exercises. 1967 edition. Preface. Appendix. Index.

A Least Squares Method for the Reduction of Free-oscillation Data

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

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Book Synopsis A Least Squares Method for the Reduction of Free-oscillation Data by : Phillip R. Wilcox

Download or read book A Least Squares Method for the Reduction of Free-oscillation Data written by Phillip R. Wilcox and published by . This book was released on 1968 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Marine Propellers and Propulsion

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Publisher : Butterworth-Heinemann
ISBN 13 : 0080971237
Total Pages : 539 pages
Book Rating : 4.0/5 (89 download)

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Book Synopsis Marine Propellers and Propulsion by : John Carlton

Download or read book Marine Propellers and Propulsion written by John Carlton and published by Butterworth-Heinemann. This book was released on 2012-10-30 with total page 539 pages. Available in PDF, EPUB and Kindle. Book excerpt: The early development of the screw propeller. Propeller geometry. The propeller environment. The ship wake field, propeller performance characteristics.

Introduction to Aircraft Aeroelasticity and Loads

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Publisher : John Wiley & Sons
ISBN 13 : 047085846X
Total Pages : 559 pages
Book Rating : 4.4/5 (78 download)

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Book Synopsis Introduction to Aircraft Aeroelasticity and Loads by : Jan Robert Wright

Download or read book Introduction to Aircraft Aeroelasticity and Loads written by Jan Robert Wright and published by John Wiley & Sons. This book was released on 2008-02-28 with total page 559 pages. Available in PDF, EPUB and Kindle. Book excerpt: Aeroelastic phenomena arising from the interaction of aerodynamic, elastic and inertia forces, and the loads resulting from flight / ground manoeuvres and gust / turbulence encounters, have a significant influence upon aircraft design. The prediction of aircraft aeroelastic stability, response and loads requires application of a range of interrelated engineering disciplines. This new textbook introduces the foundations of aeroelasticity and loads for the flexible aircraft, providing an understanding of the main concepts involved and relating them to aircraft behaviour and industrial practice. This book includes the use of simplified mathematical models to demonstrate key aeroelastic and loads phenomena including flutter, divergence, control effectiveness and the response and loads resulting from flight / ground manoeuvres and gust / turbulence encounters. It provides an introduction to some up-to-date methodologies for aeroelastics and loads modelling. It lays emphasis on the strong link between aeroelasticity and loads. It also includes provision of MATLAB and SIMULINK programs for the simplified analyses. It offers an overview of typical industrial practice in meeting certification requirements.

Airplane Aerodynamics and Performance

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Publisher : DARcorporation
ISBN 13 : 9781884885440
Total Pages : 748 pages
Book Rating : 4.8/5 (854 download)

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Book Synopsis Airplane Aerodynamics and Performance by : Jan Roskam

Download or read book Airplane Aerodynamics and Performance written by Jan Roskam and published by DARcorporation. This book was released on 1997 with total page 748 pages. Available in PDF, EPUB and Kindle. Book excerpt:

The Theory of Propellers

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ISBN 13 :
Total Pages : 184 pages
Book Rating : 4.3/5 (126 download)

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Book Synopsis The Theory of Propellers by : Theodore Theodorsen

Download or read book The Theory of Propellers written by Theodore Theodorsen and published by . This book was released on 1944 with total page 184 pages. Available in PDF, EPUB and Kindle. Book excerpt: Summary: A technical method is given for calculating the axial interference velocity of a propeller. The method involves the use of certain weight functions P, Q, and F. Numerical values for the weight functions are given for two-blade, three-blade, and six-blade propellers.

Recent Developments in Sustainable Infrastructure

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Publisher : Springer Nature
ISBN 13 : 9811545774
Total Pages : 1068 pages
Book Rating : 4.8/5 (115 download)

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Book Synopsis Recent Developments in Sustainable Infrastructure by : Bibhuti Bhusan Das

Download or read book Recent Developments in Sustainable Infrastructure written by Bibhuti Bhusan Das and published by Springer Nature. This book was released on 2020-07-03 with total page 1068 pages. Available in PDF, EPUB and Kindle. Book excerpt: This book comprises select peer-reviewed proceedings of the International Conference on Recent Developments in Sustainable Infrastructure (ICRDSI) 2019. The topics span over all major disciplines of civil engineering with regard to sustainable development of infrastructure and innovation in construction materials, especially concrete. The book covers numerical and analytical studies on various topics such as composite and sandwiched structures, green building, groundwater modeling, rainwater harvesting, soil dynamics, seismic resistance and control of structures, waste management, structural health monitoring, and geo-environmental engineering. This book will be useful for students, researchers and professionals working in sustainable technologies in civil engineering.