Zobrazeno 1 - 10
of 34
pro vyhledávání: '"Myles L. Baker"'
Publikováno v:
Composite Structures. 304:116352
Publikováno v:
Composites Part B: Engineering. 216:108847
3D through-the-thickness stitching can be used to improve interlaminar properties of polymer matrix composites (PMCs) and produce lightweight, unitized structures for cryogenic storage tanks. To fully utilize stitched composite structures for these a
Publikováno v:
58th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference.
The SpaRibs topology of an aircraft wing has a significant effect on its structural behavior and stability as well as the flutter performance. The development of additive manufacturing techniques like Electron Beam Free Form Fabrication (EBF3) has ma
Autor:
Myles L. Baker, Mohamed Jrad, Shuvodeep De, Grant Ogawa, Steven Doyle, Joe H. Robinson, Rakesh K. Kapania
Publikováno v:
17th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference.
Publikováno v:
57th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference.
A class of air vehicles known as high altitude long endurance (HALE) has gained interest for a broad range of applications. Endurance requirements generally lead to vehicles with low mass and high aspect ratio wings. Such configurations are generally
Publikováno v:
53rd AIAA Aerospace Sciences Meeting.
The paper presents a comprehensive study involving experiments and numerical simulations to measure the acoustic field in a rectangular supersonic cavity with and without a generic store. Unsteady pressure spectra measured in the empty cavity show th
Autor:
Myles L. Baker, William P. Rodden
Publikováno v:
Journal of Aircraft. 38:772-776
1.668 1.631 1.601 1.556 1.56 cD 0.0202 0.0200 0.0206 0.0242 0.0208 Separation 96.6% 93.2% 91.7% 88.0% 82% 60% chord, the predicted velocity proe les are too full. The effect of the transition on the suction side is tested by moving the transition poi
Publikováno v:
Journal of Aircraft. 36:682-688
The doublet-lattice method (DLM) has become a standard source for the aerodynamic loads in utter and dynamic response analyses of aircraft at subsonic speeds. A recent re nement to the method is based on an improvement to the integration of the
Autor:
R. D'Vari, Myles L. Baker
Publikováno v:
Journal of Aircraft. 36:156-166
An aeroelastic integrated loads subsystem (AILS) is being developed and verified for the calculation of aeroelastic loads for analysis and design. AILS will fit within the aeroelastic design optimization program. The purpose of AILS is to integrate t
Autor:
D. L. Mingori, Myles L. Baker
Publikováno v:
Journal of Guidance, Control, and Dynamics. 19:1216-1220
Modern off-line system identification methods necessarily form a system realization using a finite amount of data. The models constructed are usually of an order smaller than the actual order of the physical system because it is not practical to mode