Browsing by Subject "Major aerospace engineering."
Now showing items 1-20 of 324
-
(Texas A&M University, 1997)The engineers are primarily interested in quantities like stresses and displacements in the critical regions, the stress intensity factor at the crack-tip of an initiated crack, etc., and the error in these quantities. The ...
-
(Texas A&M University, 1974)Not available
-
(Texas A&M University, 1989)Not available
-
(Texas A&M University, 1996)Linear and nonlinear aeroelastic response is modeled with an unique test apparatus that allows for prescribed plunge and pitch motion of a wing. The addition of a control surface, combined with a personal-computer based ...
-
(Texas A&M University, 2000)The use of synthetic jet actuators for controlling the boundary layer flow and flow separation over a wing is investigated. A theory for the optimum design of actuators using motors is developed. A motor driven synthetic ...
-
(Texas A&M University, 2002)Drag reduction for aerial vehicles has a range of positive ramifications: reduced fuel consumption with the associated economic and environmental consequences, larger flight range and endurance and higher achievable flight ...
-
(Texas A&M University, 1998)The objective of the current research is to develop aphics. and demonstrate the efficacy of an adaptive multigrid coarsening strategy to accelerate the convergence of steady state solutions to convection-dominated equations. ...
-
(Texas A&M University, 1998)An adaptive mesh method for the simulation of parallel ics. Blade Vortex Interaction (BV1) with an active Trailing Edge Flap (TEF) is presented. The two-dimensional 1111-steady problem is solved by a higher order upwind ...
-
(Texas A&M University, 1988)Not available
-
(Texas A&M University, 1965)Not available
-
(Texas A&M University, 1974)Not available
-
(Texas A&M University, 2000)Aircraft agility metrics have been proposed for use to measure the performance and capability of aircraft onboard while in-flight. The sensitivity of these metrics to various types of errors and uncertainties is not ...
-
(Texas A&M University, 1998)In order to demonstrate the applicability of an All-aphics. At-once approach to a multi-disciplinary design problem, we consider the optimization of an aeroelastic, subsonic wing. As a first step, the aerodynamic and ...
-
(Texas A&M University, 1973)Not available
-
(Texas A&M University, 1993)The incremental iterative technique is implemented to solve the sensitivity equations, and, thus, improve the concept that it is possible to efficiently couple for three dimensional transonic flow about an unswept and ...
-
(Texas A&M University, 1988)Not available
-
(Texas A&M University, 1998)Current advances in semiconductor manufacturing have brought about an increasing use of thermoelectricity in a variety of applications. Most of these applications, however, have involved the steady state application of ...
-
(Texas A&M University, 1970)Not available