Download or read book Supersonic Aeroelastic Effects on Static Stability and Control Aeroelastic interaction by V W Donato written by Bell Aircraft Corporation and published by . This book was released on 1958 with total page 374 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 Thermoelastic Effects on Hypersonic Stability and Control Hypersonic aerodynamics written by James R. Batt and published by . This book was released on 1963 with total page 392 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Thermoelastic Effects on Hypersonic Stability and Control Hypersonic aeroelasticity written by James R. Batt and published by . This book was released on 1963 with total page 190 pages. Available in PDF, EPUB and Kindle. Book excerpt:

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 Thermal Effects on Static Aeroelastic Stability and Control sup Description and results of tests conducted to determine the thermally affected behavior of corrugated multiweb wing structures by J F Quinn written by Bell Aircraft Corp and published by . This book was released on 1959 with total page 214 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Proceedings of Symposium on Aerothermoelasticity written by David M. Jones and published by . This book was released on 1962 with total page 1028 pages. Available in PDF, EPUB and Kindle. Book excerpt: A symposium on Aerothermoelasticity was held to present the latest significant developments in each scientific area and engineering area that comprise the component parts of this technology. New and significant contributions were presented in four technical areas consisting of dynamic aerothermoelasticity (flutter), stability and control, thermodynamics and aerodynamics (or aerothermodynamics), and structures including material and construction concepts. Categories important and significant to each technical area are discussed state-of-the-art wise. In addition, 26 separate papers are given on items of special importance.

Download or read book Nonlinear Thermoelastic Effects on Hypersonic Stability and Control written by James R. Batt and published by . This book was released on 1964 with total page 92 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book ASD Technical Report written by and published by . This book was released on 1962 with total page 1038 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book International Aerospace Abstracts written by and published by . This book was released on 1962 with total page 502 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Active Aeroelastic Control of Supersonic Transport Aircraft written by Kevin Michael Roughen and published by . This book was released on 2009 with total page 490 pages. Available in PDF, EPUB and Kindle. Book excerpt:

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 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 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 Aero elastic Stability of Supersonic Wings written by Maurice Anthony Biot and published by . This book was released on 1947 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Aeroelastic Analysis and Testing of Supersonic Inflatable Aerodynamic Decelerators written by Christopher Lee Tanner and published by . This book was released on 2012 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt: The current limits of supersonic parachute technology may constrain the ability to safely land future robotic assets on the surface of Mars. This constraint has led to a renewed interest in supersonic inflatable aerodynamic decelerator (IAD) technology, which offers performance advantages over the DGB parachute. Two supersonic IAD designs of interest include the isotensoid and tension cone, named for their respective formative structural theories. Although these concepts have been the subject of various tests and analyses in the 1960s, 1970s, and 2000s, significant work remains to advance supersonic IADs to a technology readiness level that will enable their use on future flight missions. In particular, a review of the literature revealed a deficiency in adequate aerodynamic and aeroelastic data for these two IAD configurations at transonic and subsonic speeds. The first portion of this research amended this deficiency by testing flexible IAD articles at relevant transonic and subsonic conditions. The data obtained from these tests showed that the tension cone has superior drag performance with respect to the isotensoid, but that the isotensoid may demonstrate more favorable aeroelastic qualities than the tension cone. Additionally, despite the best efforts in test article design, there remains ambiguity regarding the accuracy of the observed subscale behavior for flight scale IADs. Due to the expense and complexity of large-scale testing, computational fluid-structure interaction (FSI) analyses will play an increasingly significant role in qualifying flight scale IADs for mission readiness. The second portion of this research involved the verification and validation of finite element analysis (FEA) and computational fluid dynamic (CFD) codes for use within an FSI framework. These verification and validation exercises lend credence to subsequent coupled FSI analyses involving more complex geometries and models. The third portion of this research used this FSI framework to predict the static aeroelastic response of a tension cone IAD in supersonic flow. Computational models were constructed to mimic the wind tunnel test articles and flow conditions. Converged FSI responses computed for the tension cone agreed reasonably well with wind tunnel data when orthotropic material models were used and indicated that current material models may require unrealistic input parameters in order to recover realistic deformations. These FSI analyses are among the first results published that present an extensive comparison between FSI computational models and wind tunnel data for a supersonic IAD.

Download or read book Secondary Flow Fields Embedded in Hypersonic Shock Layers written by Alvin Seiff and published by . This book was released on 1962 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt: