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...
Inviscid Small Disturbance Theory for Nonuniform Transonic Flows, (2005)
The classical inviscid theory of irrotational small three dimensional perturbations in uniform transonic flows is extended to include arbitrarily-nonuniform non-adiabatic two dimensional or...
Analytic Investigation of Transonic Normal Shock-Boundary Layer Interaction. (2002)
Advances in inviscid transonic flow field computational capability and supercritical airfoil design make it important to understand of the the physics of normal shock-boundary layer interactions. In...
An Idealized Theory of Transonic Normal Shock-Boundary Layer Interaction. (2002)
A simplified two-layer theoretical model of a transonic normal shock interacting with an unseparated laminar or turbulent boundary layer is studied. It constitutes an extension of Isien and Finston's...
Function subprograms for the computation of the digamma function and generalized zeta function are presented. Some new analytic results are given, and tables of 20 place values of the functions are...
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...