Author

Shreekant Agrawal

Observed names: Agrawal, Shreekant, SHREEKANT AGRAWAL

Institution: Northrop Grumman (United States)

Observed institutions: Boeing (United States), Northrop Grumman (United States), McDonnel Douglas (United States), McDonnel Aircraft (United States)

OpenAlex ID: A5110048504

Data Summary from the First AIAA Computational Fluid Dynamics Drag Prediction Workshop

2003 · David W. Levy, Thomas Zickuhr, et al. · Journal of Aircraft · 110

Method for perturbing multiblock patched grids in aeroelastic and design optimization applications

1997 · Peter Hartwich, Shreekant Agrawal · AIAA Computational Fluid Dynamics Conference · 49

Numerical investigation of vortex breakdown on a delta wing

1992 · Shreekant Agrawal, Raymond Matt Barnett, et al. · AIAA Journal · 47

Navier-Stokes calculations on multi-element airfoils using a chimera-based solver

1993 · Donald W. Jasper, Shreekant Agrawal, et al. · NASA Technical Reports Server (NASA) · 7

A numerical study of control surface buzz using computational fluid dynamic methods

1992 · DENNIS FUGLSANG, LARRY BRASE, et al. · AIAA Applied Aerodynamics Conference · 6

Evaluation of Euler solvers for transonic wing-fuselage geometries

1991 · Shreekant Agrawal, Son Frangois Creasman, et al. · Journal of Aircraft · 6

Supersonic boundary-layer stability analysis on an aircraft wing

1991 · Shreekant Agrawal, Thomas A. Kinard, et al. · Journal of Aircraft · 6

Aerospace vehicle MDO shape optimization using ADIFOR 3.0 gradients

2000 · Pichuraman Sundaram, Shreekant Agrawal, et al. · AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference (MAO) · 5

Data Summary from First AIAA Computational Fluid Dynamics Drag Prediction Workshop

2003 · David W. Levy, Tom Zickuhr, et al. · Journal of Aircraft · 4

Drag prediction using nonlinear computational methods

2000 · Shreekant Agrawal, Robert Narducci · AIAA Aerospace Sciences Meeting and Exhibit · 4

Fast and Accurate Aerodynamic Predictions Using Unsteady CFD

2019 · Pichuraman Sundaram, Shreekant Agrawal · AIAA AVIATION Forum · 3

Supersonic boundary layer stability analysis with and without suction on aircraft wings

1989 · Shreekant Agrawal, Tom A. Kinard, et al. · NASA Technical Reports Server (NASA) · 2

AIAA 2002-0841 Summary of Data from the

2002 · David Levy, Tom Zickuhr, et al. · 1

Supersonic Aerodynamic Design Improvements of an Arrow-Wing HSCT Configuration Using Nonlinear Point Design Methods

1999 · Eric R. Unger, James O. Hager, et al. · NASA Technical Reports Server (NASA) · 1

Asymptotic Theory of an Unseparated Supersonic Turbulent Boundary Layer At a Compression Corner.

1983 · Shreekant Agrawal · Deep Blue (University of Michigan) · 1

Summary of Data from the First AIAA CFD Drag Prediction Workshop

2002 · David Levy, Tom Zickuhr, et al. · NASA STI/Recon Technical Report N

CFD Data Generation Process for Nonlinear Loads

1999 · Alan E. Arslan, Todd Magee, et al. · NASA Technical Reports Server (NASA)

Configuration Aerodynamics: Past - Present - Future

1999 · Richard M. Wood, Shreekant Agrawal, et al. · NASA Technical Reports Server (NASA)

Experimental Investigation of a Point Design Optimized Arrow Wing HSCT Configuration

1999 · Robert Narducci, P. Sundaram, et al. · NASA Technical Reports Server (NASA)

Orthonormal functions for airfoil and wing parametrization

1996 · Peter Hartwich, Shreekant Agrawal · AIAA Applied Aerodynamics Conference

Investigation of Aerodynamic Stall Alleviation on a Swept Planform Wing Using Leading Edge Modifications

1981 · Roger W Van Gunst, Shreekant Agrawal, et al. · Defense Technical Information Center (DTIC)

Works count: 24

Citation count: 252

H-index: 6

I10-index: 3