Shreekant Agrawal

AIAA 2002-0841 Summary of Data from the

Richard A. Wahls, Shahyar Pirzadeh, Michael J. Hemsch, 2002 .

CFD Data Generation Process for Nonlinear Loads

Neal M. Chaderjian, Bala Bharadvaj, Eric Unger, 1999 .

Experimental Investigation of a Point Design Optimized Arrow Wing HSCT Configuration

Pichuraman Sundaram, Shreekant Agrawal, Alan E. Arslan, 1999 .

Aerospace vehicle MDO shape optimization using ADIFOR 3.0 gradients

Pichuraman Sundaram, James O. Hager, Shreekant Agrawal, 2000 .

Configuration Aerodynamics: Past - Present - Future

Daniel P. Bencze, Richard M. Wood, Douglas L. Wilson, 1999 .

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

Eric Unger, James O. Hager, Shreekant Agrawal, 1999 .