A. Goel T, C. A. Baker, B. Grossman, W. H. Mason, ...
We describe a problem solving environment (PSE) named VizCraft that aids aircraft designers during the conceptual design stage. At this stage, an aircraft design is defined by a vector of 10-30...
Analysis of the Interaction of a Weak Normal Shock Wave with a Turbulent Boundary Layer, (2002)
The method of matched asymptotic expansions is used to analyze the interaction of a normal shock wave with an unseparated turbulent boundary layer on a flat surface at transonic speeds. The theory...
The Viscous Transonic Flow over Two-Element Airfoil Systems. (2002)
A numerical procedure has been developed to compute the transonic viscous-inviscid interacting flow field about airfoils with leading edge slats or trailing edge flaps. The inviscid theory utilizes...
An Analysis of the Inviscid Transonic Flow over Two-Element Airfoil Systems. (2002)
This report describes the development of a method for numerically computing the inviscid transonic flow field over an airfoil with a leading-edge slat or a trailing-edge flap. The approach is to...
A. Goel, C.A. Baker, C.A. Shaffer, C. A. Sha#er, B. Grossman, W.H. Mason, ...
We describe a problem solving environment named VizCraft that aids aircraft designers during the conceptual design stage. At this stage, an aircraft design is defined by a vector of 10-30 parameters....
Multidisciplinary Design Optimization of a Strut-Braced Wing Transonic Transport (2000)
J.F. Gundlach IV, P-a. Tétrault, F. Gern, A. Nagshineh-pour, A. Ko, ...
Recent transonic airliner designs have generally converged upon a common cantilever low-wing configuration. It is unlikely that further large strides in performance are possible without a significant...
VizCraft: A Multidimensional Visualization Tool for Aircraft Configuration Design (1999)
A. Goel, C. Baker, C. A. Shaffer, B. Grossman, R. T. Haftka, W.H. Mason, ...
We describe a visualization tool to aid aircraft designers during the conceptual design stage. We define the design for an aircraft by a vector of 10-30 parameters. The goal is to find a vector that...
Position Location Analysis. (1998)
Sakson,P., Grossman,B., Breda,J.
PRECISION, AIRCRAFT SURVEILLANCE AND COLLISION AVOIDANCE SYSTEM. The real time data processing and display system developed makes use of a PDP11 minicomputer and a CRT display. These equipments have...
M.: Multidisciplinary Design Optimization of a Strut-Braced Wing Aircraft (1998)
Joel M. Grasmeyer, B. Grossman, J. A. Schetz, Joel M. Grasmeyer, Joel M. Grasmeyer
The objective of this study is to use Multidisciplinary Design Optimization (MDO) to investigate the use of truss-braced wing concepts in concert with other advanced technologies to obtain a...
Dependence Of Optimal Structural Weight On Aerodynamic Shape For A High Speed Civil Transport (1996)
V. Balabanov, M. Kaufman, D. L. Knill, D. Haim, O. Golovidov, A. A. Giunta, ...
A procedure for generating a customized weight function for wing bending material weight of the High Speed Civil Transport (HSCT) is described. The weight function is based on the shape parameters. A...
Huddleston Development Of, E. J. Haug, K. K. Choi, V. Komkov, R. Narducci, ...
u, and V. M. Korivi, Sensitivity Analysis, Approximate Analysis and Design Optimization for Internal and External Viscous Flows, in Proceedings of AIAA Aircraft Design Systems and Operations Meeting,...
Glueball-Like Screening Masses in Pure SU(3) at Finite Temperatures (1993)
Grossman, B., Gupta, Sourendu, Heller, U. M., Karsch, F.
We investigate the finite-temperature excitation spectrum in the gluon sector of $SU(3)$ pure gauge theory through measurements of screening masses in correlations of loop operators. We develop the...
Directional solidification in two and three dimensions (1993)
Grant, M., Grossman, B., Elder, K. R., Kosterlitz, J. M.
A symmetric phase-field model is used to study directional solidification in two and three dimensions. Numerical evidence of tip-splitting, breathing modes, solitary modes, and other non-steady-state...
Kinetic roughening of interfaces in driven systems (1991)
Grant, M., Grossman, B., Gui, H.
We study the dynamics of an interface driven far from equilibrium in three dimensions. First we derive the Kardar-Parisi-Zhang equation from the Langevin equation for a system with a nonconserved...
Crossover scaling in the dynamics of driven systems (1990)
Grant, M., Guo, H., Grossman, B.
We study growing interfaces in two- and three-dimensional systems by the numerical integration of the Kardar-Parisi-Zhang equation and the Monte Carlo simulation of a solid-on-solid model with...
Monte Carlo renormalization-group study of self-organized criticality (1990)
Grant, M., Grossman, B., Guo, H.
We have studied a class of dynamical models exhibiting self-organized criticality, which have recently been introduced by Bak, Tang, and Wiesenfeld [Phys. Rev. Lett. 59, 381 (1987)] by the Monte...
Kinetics of interface growth in driven systems (1990)
Grant, M., Guo, G., Grossman, B.
We study growing interfaces by the numerical simulation of several three-dimensional systems: the Kardar-Parisi-Zhang equation, a discrete variant of that model, and a solid-on-solid model with...
AN ANALYSIS OF THE LEADING-EDGE SINGULARITY IN TRANSONIC SMALL-DISTURBANCE THEORY (1978)
KEYFITZ, B. L., MELNIK, R. E., GROSSMAN, B.
We consider in detail the behaviour of solutions of the transonic small-disturbance equation near the leading edge of a smooth blunt-nosed airfoil at incidence. The character of the leading-edge...