Download or read book Aeroelastic Stability of a Membrane in Supersonic Flow written by John Merle Montgomery and published by . This book was released on 1967 with total page 48 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book On the Aeroelastic Stability of Orthotropic Wings and Panels in Supersonic Flow written by Adolf Abraham Perlmutter and published by . This book was released on 1960 with total page 158 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Aeroelastic Stability of Supersonic Nozzles with Separated Flow written by L. O. Pekkari and published by . This book was released on 1993 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Aeroelastic Vibrations and Stability of Plates and Shells written by Sergey D. Algazin and published by Walter de Gruyter GmbH & Co KG. This book was released on 2014-12-11 with total page 234 pages. Available in PDF, EPUB and Kindle. Book excerpt: Back-action of aerodynamics onto structures such as wings cause vibrations and may resonantly couple to them, thus causing instabilities (flutter) and endangering the whole structure. By careful choices of geometry, materials and damping mechanisms, hazardous effects on wind engines, planes, turbines and cars can be avoided. Besides an introduction into the problem of flutter, new formulations of flutter problems are given as well as a treatise of supersonic flutter and of a whole range of mechanical effects. Numerical and analytical methods to study them are developed and applied to the analysis of new classes of flutter problems for plates and shallow shells of arbitrary plane form. Specific problems discussed in the book in the context of numerical simulations are supplemented by Fortran code examples (available on the website).

Download or read book Manual on Aeroelasticity written by North Atlantic Treaty Organization. Advisory Group for Aeronautical Research and Development. Structures and Materials Panel and published by . This book was released on 1960 with total page 520 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Some Recent Experimental Studies on the Aeroelastic Stability of Thin Cylindrical Shells Pt i Experimental Study of the Supersonic Flow Field Over an Aeroelastic Ogive written by P. L. Daily and published by . This book was released on 1970 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Supersonic Aeroelastic Effects on Static Stability and Control written by Ivan Rattinger and published by . This book was released on 1960 with total page 325 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Principles of Aeroelasticity written by Raymond L. Bisplinghoff and published by Courier Corporation. This book was released on 2002-01-01 with total page 554 pages. Available in PDF, EPUB and Kindle. Book excerpt: Summary and general methods of constructing static and dynamic equations, dealing with the laws of mechanics for heated elastic solids, forms of aerodynamic operators, structural operators, much more. 1962 edition.

Download or read book Approximation Methods for Aeroelastic Systems in High Supersonic Flow written by Melvin B. Zisfein and published by . This book was released on 1960 with total page 93 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book An Analytical and Experimental Investigation of the Aeroelastic Stability of Cylindrical Shells at the Subsonic and Supersonic Mach Numbers written by Walter Julian Horn and published by . This book was released on 1972 with total page 318 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Development of Harmonic Panel Methods for Aeroelastic Applications to Elastic Bodies and Body Fin Combinations in Supersonic Flow written by D. D. Liu and published by . This book was released on 1989 with total page 201 pages. Available in PDF, EPUB and Kindle. Book excerpt: Recent development of several unsteady supersonic methods for computations of airloads for elastic bodies of revolution, asymmetric bodies and body wing configurations are reported. These methods include the Harmonic Potential Panel (HPP) method, the Bundle Triplet Method (BTM) and the combined method of BTM and the Harmonic Gradient Method (HGM) for body wing combinations. All methods are based on the generic Harmonic Gradient (H-G) model, which is essential in providing accurate solutions in the full frequency domain and the low Mach number range. Extensive comparisons of computed results obtained from these methods show good correlations with existing data. Comparison examples range from simple cones and ogive bodies to Saturn SA-1 configuration, to the cylindrical panel membrance and to the NACA wing-body combinations. Cases computed yield steady and unsteady pressures, generalized forces, stability derivatives, aerodynamic dampings and divergence and flutter boundaries for these configurations. The developed methods have been validated with existing theories or measured data. For supersonic aeroelastic analysis, these methods yield results that are accurate and cost-effective, thus rendering them very favorable for technology transfer and industry applications. Keywords: Unsteady aerodynamics, Supersonic flow, Aeroelasticity. (mjm).

Download or read book Supersonic Aeroelastic Effects on Static Stability and Control Pt 2 Structures written by Ivan Rattinger and published by . This book was released on 1960 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book AGARD Advisory Report written by and published by . This book was released on 1965 with total page 186 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Applied Mechanics Reviews written by and published by . This book was released on 1974 with total page 592 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book OAR Research Review written by United States. Air Force. Office of Aerospace Research and published by . This book was released on 1968 with total page 528 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Research Review written by and published by . This book was released on 1969-11 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Research Review written by United States. Air Force. Office of Aerospace Research and published by . This book was released on 1969 with total page 346 pages. Available in PDF, EPUB and Kindle. Book excerpt: