Through-silicon-via-aware prediction and physical design for multi-granularity 3D integrated circuits

The main objective of this research is to predict the wirelength, area, delay, and power of multi-granularity three-dimensional integrated circuits (3D ICs), to develop physical design methodologies and algorithms for the design of multi-granularity 3D ICs, and to investigate the impact of through-silicon vias (TSVs) on the quality of 3D ICs. This dissertation supports these objectives by addressing six research topics. The first pertains to analytical models that predict the interconnects of multi-granularity 3D ICs, and the second focuses on the development of analytical models of the capacitive coupling of TSVs. The third and the fourth topics present design methodologies and algorithms for the design of gate- and block-level 3D ICs, and the fifth topic pertains to the impact of TSVs on the quality of 3D ICs. The final topic addresses topography variation in 3D ICs. The first section of this dissertation presents TSV-aware interconnect prediction models for multi-granularity 3D ICs. As previous interconnect prediction models for 3D ICs did not take TSV area into account, they were not capable of predicting many important characteristics of 3D ICs related to TSVs. This section will present several previous interconnect prediction models that have been improved so that the area occupied by TSVs is taken into account. The new models show numerous important predictions such as the existence of the number of TSVs minimizing wirelength. The second section presents fast estimation of capacitive coupling of TSVs and wires. Since TSV-to-TSV and TSV-to-wire coupling capacitance is dependent on their relative locations, fast estimation of the coupling capacitance of a TSV is essential for the timing optimization of 3D ICs. Simulation results show that the analytical models presented in this section are sufficiently accurate for use at various design steps that require the computation of TSV capacitance. The third and fourth sections present design methodologies and algorithms for gate- and block-level 3D ICs. One of the biggest differences in the design of 2D and 3D ICs is that the latter requires TSV insertion. Since no widely-accepted design methodology designates when, where, and how TSVs are inserted, this work develops and presents several design methodologies for gate- and block-level 3D ICs and physical design algorithms supporting them. Simulation results based on GDSII-level layouts validate the design methodologies and present evidence of their effectiveness. The fifth section explores the impact of TSVs on the quality of 3D ICs. As TSVs become smaller, devices are shrinking, too. Since the relative size of TSVs and devices is more critical to the quality of 3D ICs than the absolute size of TSVs and devices, TSVs and devices should be taken into account in the study of the impact of TSVs on the quality of 3D ICs. In this section, current and future TSVs and devices are combined to produce 3D IC layouts and the impact of TSVs on the quality of 3D ICs is investigated. The final section investigates topography variation in 3D ICs. Since landing pads fabricated in the bottommost metal layer are attached to TSVs, they are larger than TSVs, so they could result in serious topography variation. Therefore, topography variation, especially in the bottommost metal layer, is investigated and two layout optimization techniques are applied to a global placement algorithm that minimizes the topography variation of the bottommost metal layer of 3D ICs.PhDCommittee Chair: Lim, Sung Kyu; Committee Member: Bakir, Muhannad; Committee Member: Kim, Hyesoon; Committee Member: Lee, Hsien-Hsin Sean; Committee Member: Mukhopadhyay, Saiba

Distributed Propulsion Vehicles

Since the introduction of large jet-powered transport aircraft, the majority of these vehicles have been designed by placing thrust-generating engines either under the wings or on the fuselage to minimize aerodynamic interactions on the vehicle operation. However, advances in computational and experimental tools along with new technologies in materials, structures, and aircraft controls, etc. are enabling a high degree of integration of the airframe and propulsion system in aircraft design. The National Aeronautics and Space Administration (NASA) has been investigating a number of revolutionary distributed propulsion vehicle concepts to increase aircraft performance. The concept of distributed propulsion is to fully integrate a propulsion system within an airframe such that the aircraft takes full synergistic benefits of coupling of airframe aerodynamics and the propulsion thrust stream by distributing thrust using many propulsors on the airframe. Some of the concepts are based on the use of distributed jet flaps, distributed small multiple engines, gas-driven multi-fans, mechanically driven multifans, cross-flow fans, and electric fans driven by turboelectric generators. This paper describes some early concepts of the distributed propulsion vehicles and the current turboelectric distributed propulsion (TeDP) vehicle concepts being studied under the NASA s Subsonic Fixed Wing (SFW) Project to drastically reduce aircraft-related fuel burn, emissions, and noise by the year 2030 to 2035

A time-accurate high-resolution TVD scheme for solving the Navier-Stokes equations

A total variation diminishing (TVD) scheme has been developed and incorporated into an existing time-accurate high-resolution Navier-Stokes code. The accuracy and the robustness of the resulting solution procedure have been assessed by performing many calculations in four different areas: shock tube flows, regular shock reflection, supersonic boundary layer, and shock boundary layer interactions. These numerical results compare well with corresponding exact solutions or experimental data