Multi-Fidelity Analysis of Corrugated-Core Sandwich Panels for Integrated Thermal Protection Systems

Multi-Fidelity Analysis of Corrugated-Core Sandwich Panels for Integrated Thermal Protection Systems

Author(s):

Sharma, Anurag ( Department of Mechanical and Aerospace Engineering, University of Florida, PO Box 116250, Gainesville, FL 32611-6250 )
Sankar, Bhavani V
Haftka, Raphael T

Publication title:

AIAA meeting papers on disc

Title of ser.:

AIAA Paper : AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference

Ser. no.:

2009

Pub. Year:

2009

No.:

2009-2201

Paper no.:

AIAA Paper 2009-2201

Pages:

24

Pub. info.:

Reston, Va.: American Institute of Aeronautics and Astronautics

ISSN:

10877215

Language:

English

Call no.:

A07400/200905

Type:

Technical Paper

Link(DOI, etc.)

http://doi.org/10.2514/6.2009-2201

Details

TDL ID:	ZA00066595
Series ID:	PA00000154
Conf. info. (Name):	AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference
Conf. info. (Number):	50th
Conf. info. (Venue):	Palm Springs, California
Conf. info. (Date):	2009.05.04-2009.05.07
Note for article:	50th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference 17th 4-7 May 2009, Palm Springs, California

Similar Items:

1 Technical Paper (Student Paper) Analysis and Design of Corrugated-Core Sandwich Panels for Thermal Protection Systems of Space Vehicles S. Bapanapalli, O. Martinez, C. Gogu, B. Sankar, R. Haftka, M. Blosser American Institute of Aeronautics and Astronautics	7 Technical Paper Probabilistic Optimization of Integrated Thermal Protection System S. Kumar, D. Villanueva, B. Sankar, R. Haftka American Institute of Aeronautics and Astronautics
2 Technical Paper Multi-Fidelity Design of an Integrated Thermal Protection System for Spacecraft Reentry A. Sharma, C. Gogu, O. Martinez, B. Sankar, R. Haftka American Institute of Aeronautics and Astronautics	8 Technical Paper Comparison of Materials for Integrated Thermal Protection Systems for Spacecraft Reentry C. Gogu, S. Bapanapalli, R. Haftka, B. Sankar American Institute of Aeronautics and Astronautics
3 Technical Paper Micromechanical Analysis of Composite Truss-Core Sandwich Panels for Integral Thermal Protection Systems O. Martinez, S. Bapanapalli, B. Sankar, R. Haftka, M. Blosser American Institute of Aeronautics and Astronautics	9 Technical Paper Analysis of TPS Sandwich Panel with Foam Core Zhu, H., Sankar, B. American Institute of Aeronautics and Astronautics
4 Technical Paper Structural optimization of a hat stiffened panel by response surface techniques Vitali, Roberto, Park, Oung, Haftka, Raphael T., Sankar, Bhavani V. American Institute of Aeronautics and Astronautics	10 Technical Paper Integration of finite element analysis program and panel design program Venkataraman, Satchi, Haftka, Raphael T. American Institute of Aeronautics and Astronautics
5 Technical Paper Optimal Weight of Cracked Composite Panels By An Equivalent Strain Constraint Papila,Melih, Vitali,Roberto, Haftka,Raphael T., Sankar,Bhavani V. American Institute of Aeronautics and Astronautics	11 Technical Paper Evaluation of Integrated Sandwich TPS Design with Metal Foam Core for Launch Vehicles Zhu, H., Sankar, B., Haftka, R., Blosser, M. American Institute of Aeronautics and Astronautics
6 Technical Paper Analytical and experimental study of a blade stiffened panel in axial compression Park, Oung, Haftka, Raphael T., Sankar, Bhavani V., Nagendra, Somanath American Institute of Aeronautics and Astronautics	12 Technical Paper Separable Sampling of the Limit State for Accurate Monte Carlo Simulation Ravishankar, Bharani, Smarslok, Benjamin, Haftka, Raphael, Sankar, Bhavani American Institute of Aeronautics and Astronautics

1

2

3

4

5

6

7

8

9

10

11

12