Zobrazeno 1 - 10
of 10
pro vyhledávání: '"Theresa C. Shafer"'
Autor:
Theresa C. Shafer, Benjamin P. Hallissy, Nathan S. Hariharan, Cynthia Dahl, David Hine, James R. Forsythe, Jennifer Abras, Joseph P. Laiosa
Publikováno v:
Computing in Science & Engineering. 18:52-62
A successful fielding of computation-based engineering (CBE) software requires quality assurance to be built into the fabric of capability development and deployment processes. Good software quality is an emergent property of the healthy interplay am
Publikováno v:
2018 Applied Aerodynamics Conference.
Autor:
Eric Lynch, Jim Forsythe, Theresa C. Shafer, Benjamin P. Hallissy, David Hine, Bradford E. Green
Publikováno v:
54th AIAA Aerospace Sciences Meeting.
Publikováno v:
53rd AIAA Aerospace Sciences Meeting.
Autor:
Jonathan Dansie, Sally A. Viken, Noah Favaregh, Nathan Williams, Theresa C. Shafer, Cale Zeune, C. Eric Lynch
Publikováno v:
52nd Aerospace Sciences Meeting.
Computational Fluid Dynamic (CFD) methods were used to determine the basic aerodynamic, performance, and stability and control characteristics of the unmanned air vehicle (UAV), Kahu. Accurate and timely prediction of the aerodynamic characteristics
Publikováno v:
52nd Aerospace Sciences Meeting.
Publikováno v:
52nd Aerospace Sciences Meeting.
Kestrel is a fixed-wing computational based engineering product of the CREATE-AV program. Kestrel offers many advanced features that can be very useful for Navy applications. Some of these features include: modeling an aircraft in a prescribed maneuv
Publikováno v:
52nd Aerospace Sciences Meeting.
Autor:
Joseph P. Laiosa, David Hine, Cynthia Dahl, Nathan S. Hariharan, Jennifer Abras, Chad S. Lillian, James R. Forsythe, Theresa C. Shafer, Benjamin P. Hallissy
Publikováno v:
52nd Aerospace Sciences Meeting.
Autor:
Theresa C. Shafer, Bradford E. Green
Publikováno v:
48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition.
A Computational Fluid Dynamic approach has been applied to generating a flight database for Unmanned Aerial Vehicle systems to be used in the flight certification process. There is a need to build confidence in producing computational solutions of sm