Static Aeroelastic Effects on the Flutter of a Supercritical Wing

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ISBN 13 :
Total Pages : 20 pages
Book Rating : 4.:/5 (317 download)

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Book Synopsis Static Aeroelastic Effects on the Flutter of a Supercritical Wing by :

Download or read book Static Aeroelastic Effects on the Flutter of a Supercritical Wing written by and published by . This book was released on 1987 with total page 20 pages. Available in PDF, EPUB and Kindle. Book excerpt: It is well known that wings with supercritical airfoils generally have lower transonic flutter speeds than similar wings with conventional airfoils and that small increases in angle of attack from zero and the accompanying static aeroelastic deformations have further detrimental effects on transonic flutter. This paper presents results of an effort to calculate the effects of angle of attack and the associated aeroelastic deformation on the flutter of a highly swept supercritical wing (TF-8A) by use of modified strip analysis. The spanwise distributions of steady-state section life-curve slope and aerodynamic calculations for as input for these calculations were obtained from static aeroelastic calculations for the wing by use of hte FL022 transonic code and an assumed dynamic pressure. The process is iterative so that flutter can be obtained at the same dynamic pressure as that used to calculate the statically deformed shape and loading about which the flutter oscillation occurs (matched conditions). Investigation results show that the unconventional backward turn of the transonic dip in the experimental flutter boundary for angles of attack greater than zero is caused by variations in mass ratio and not by static aeroelastic deformation, although inclusion of the latter appears to be required for quantitative accuracy in the calculations. For the very high subsonic Mach numbers of this investigation, quantitative accuracy will also require inclusion of viscous effects on shock strength and location.

Measured and Calculated Effects of Angle of Attack on the Transonic Flutter of a Supercritical Wing

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ISBN 13 :
Total Pages : 30 pages
Book Rating : 4.:/5 (317 download)

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Book Synopsis Measured and Calculated Effects of Angle of Attack on the Transonic Flutter of a Supercritical Wing by :

Download or read book Measured and Calculated Effects of Angle of Attack on the Transonic Flutter of a Supercritical Wing written by and published by . This book was released on 1982 with total page 30 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Static Aeroelastic Effects on High Performance Aircraft

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ISBN 13 :
Total Pages : 186 pages
Book Rating : 4.:/5 (227 download)

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Book Synopsis Static Aeroelastic Effects on High Performance Aircraft by : ADVISORY GROUP FOR AEROSPACE RESEARCH AND DEVELOPMENT NEUILLY-SUR-SEINE (FRAN CE)

Download or read book Static Aeroelastic Effects on High Performance Aircraft written by ADVISORY GROUP FOR AEROSPACE RESEARCH AND DEVELOPMENT NEUILLY-SUR-SEINE (FRAN CE) and published by . This book was released on 1987 with total page 186 pages. Available in PDF, EPUB and Kindle. Book excerpt: Modern high performance aircraft designs tend to employ very thin airfoils having a degree and a distribution of stiffness far from the ideal; in consequence, there is a loss of control effectiveness and maneuverability. Moreover, the introduction of the highly forward-swept-wing planform poses a static aeroelastic effect of fundamental importance; these effects are felt at model as well as at full scale. This meeting was organized not only to review instances of these problems but to see how successfully modern tools for structural and aeroelastic analysis can be applied. The individual papers of the meeting cover many aspects of static aeroelasticity not only for military aircraft but also for modern transport aircraft. The various papers also address problems and recent progress in wind tunnel model testing, in particular measurement of static deformations on wind tunnel models. Keywords: Flutter, Supercritical wings, Aerodynamic loading, Jet fighters, Aerodynamic trim, Symposia, Maneuverability, Sweptforward wings, Aeroelasticity, Aerostatics, Structural analysis, Military aircraft, Transport aircraft, Wind tunnel models.

Supercritical Wing Flutter

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ISBN 13 :
Total Pages : 238 pages
Book Rating : 4.:/5 (227 download)

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Book Synopsis Supercritical Wing Flutter by : J. A. McGrew

Download or read book Supercritical Wing Flutter written by J. A. McGrew and published by . This book was released on 1978 with total page 238 pages. Available in PDF, EPUB and Kindle. Book excerpt: Transonic methods for correcting subsonic oscillatory aerodynamic influence coefficients (AIC's) based on the Doublet Lattice Method for use in flutter and dynamic response analyses of supercritical wings are developed and applied to a TF-8A flutter model and the YC-15II prototype aircraft. The effects of static aeroelasticity are included and evaluated. Reynolds number effects on test results are discussed. Correlation of improved methods showed good agreement with test results. For the two applications included, the steady corrections dominated the unsteady corrections. In the process of developing transonic corrections a new transonic lifting surface theory (currently two-dimensional) is presented, explored and correlated using the NLR 7301 airfoil. The effects of shock wave motion are included in the theory. (Author).

Scientific and Technical Aerospace Reports

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ISBN 13 :
Total Pages : 836 pages
Book Rating : 4.:/5 (31 download)

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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 1994 with total page 836 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Transonic Unsteady Aerodynamics and Aeroelasticity, 1987

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ISBN 13 :
Total Pages : 684 pages
Book Rating : 4.3/5 (126 download)

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Book Synopsis Transonic Unsteady Aerodynamics and Aeroelasticity, 1987 by :

Download or read book Transonic Unsteady Aerodynamics and Aeroelasticity, 1987 written by and published by . This book was released on 1989 with total page 684 pages. Available in PDF, EPUB and Kindle. Book excerpt:

An Analysis of the Effects of Aeroelasticity on Static Longitudinal Stability and Control of a Swept-back-wing Airplane

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ISBN 13 :
Total Pages : 50 pages
Book Rating : 4.3/5 (91 download)

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Book Synopsis An Analysis of the Effects of Aeroelasticity on Static Longitudinal Stability and Control of a Swept-back-wing Airplane by : Richard B. Skoog

Download or read book An Analysis of the Effects of Aeroelasticity on Static Longitudinal Stability and Control of a Swept-back-wing Airplane written by Richard B. Skoog and published by . This book was released on 1951 with total page 50 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Application of a Transonic Potential Flow Code to the Static Aeroelastic Analysis of Three-dimensional Wings

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ISBN 13 :
Total Pages : 16 pages
Book Rating : 4.:/5 (317 download)

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Book Synopsis Application of a Transonic Potential Flow Code to the Static Aeroelastic Analysis of Three-dimensional Wings by :

Download or read book Application of a Transonic Potential Flow Code to the Static Aeroelastic Analysis of Three-dimensional Wings written by and published by . This book was released on 1982 with total page 16 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Prediction of Transonic Flutter for a Supercritical Wing by Modified Strip Analysis and Comparison with Experiment

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ISBN 13 :
Total Pages : 36 pages
Book Rating : 4.:/5 (317 download)

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Book Synopsis Prediction of Transonic Flutter for a Supercritical Wing by Modified Strip Analysis and Comparison with Experiment by :

Download or read book Prediction of Transonic Flutter for a Supercritical Wing by Modified Strip Analysis and Comparison with Experiment written by and published by . This book was released on 1981 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Monthly Catalogue, United States Public Documents

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ISBN 13 :
Total Pages : 1644 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis Monthly Catalogue, United States Public Documents by :

Download or read book Monthly Catalogue, United States Public Documents written by and published by . This book was released on 1991 with total page 1644 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Monthly Catalog of United States Government Publications

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ISBN 13 :
Total Pages : 1200 pages
Book Rating : 4.:/5 (891 download)

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Book Synopsis Monthly Catalog of United States Government Publications by :

Download or read book Monthly Catalog of United States Government Publications written by and published by . This book was released on with total page 1200 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Predicted Static Aeroelastic Effects on Wings with Supersonic Leading Edges and Streamwise Tips [with List of References]

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ISBN 13 :
Total Pages : 38 pages
Book Rating : 4.:/5 (459 download)

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Book Synopsis Predicted Static Aeroelastic Effects on Wings with Supersonic Leading Edges and Streamwise Tips [with List of References] by :

Download or read book Predicted Static Aeroelastic Effects on Wings with Supersonic Leading Edges and Streamwise Tips [with List of References] written by and published by . This book was released on 1959 with total page 38 pages. Available in PDF, EPUB and Kindle. Book excerpt:

NASA SP.

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Total Pages : 654 pages
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Book Synopsis NASA SP. by :

Download or read book NASA SP. written by and published by . This book was released on 1992 with total page 654 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Further Investigations of the Aeroelastic Behavior of the AFW Wind-tunnel Model Using Transonic Small Disturbance Theory

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Total Pages : 16 pages
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Book Synopsis Further Investigations of the Aeroelastic Behavior of the AFW Wind-tunnel Model Using Transonic Small Disturbance Theory by :

Download or read book Further Investigations of the Aeroelastic Behavior of the AFW Wind-tunnel Model Using Transonic Small Disturbance Theory written by and published by . This book was released on 1992 with total page 16 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Measured and Calculated Effects of Angle of Attack on the Transonic Flutter of a Supercritical Wing

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Publisher : Createspace Independent Publishing Platform
ISBN 13 : 9781725156456
Total Pages : 34 pages
Book Rating : 4.1/5 (564 download)

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Book Synopsis Measured and Calculated Effects of Angle of Attack on the Transonic Flutter of a Supercritical Wing by : National Aeronautics and Space Administration (NASA)

Download or read book Measured and Calculated Effects of Angle of Attack on the Transonic Flutter of a Supercritical Wing written by National Aeronautics and Space Administration (NASA) and published by Createspace Independent Publishing Platform. This book was released on 2018-08-13 with total page 34 pages. Available in PDF, EPUB and Kindle. Book excerpt: For abstract see A82-30143. Yates, E. C., Jr. and Wynne, E. C. and Farmer, M. G. Langley Research Center NASA-TM-83276, NAS 1.15:83276 RTOP 505-33-53-07...

Scientific and Technical Information Output of the Langley Research Center for Calendar Year 1986

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ISBN 13 :
Total Pages : 270 pages
Book Rating : 4.:/5 (317 download)

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Book Synopsis Scientific and Technical Information Output of the Langley Research Center for Calendar Year 1986 by : Langley Research Center. Research Information and Applications Division

Download or read book Scientific and Technical Information Output of the Langley Research Center for Calendar Year 1986 written by Langley Research Center. Research Information and Applications Division and published by . This book was released on 1987 with total page 270 pages. Available in PDF, EPUB and Kindle. Book excerpt:

AGARD Index of Publications

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ISBN 13 :
Total Pages : 410 pages
Book Rating : 4.3/5 (243 download)

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Book Synopsis AGARD Index of Publications by : North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development

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