درخواست مقاله يا پسورد AIAA

1.
82%
2007 Subject Index

. .
Journal of Aircraft 2007
0021-8669 vol.44 no.6 (2091-2099)


2.
80%
Probabilistic Approach to Damage Tolerance Design of Aircraft Composite Structures

K. Lin and A. Styuart, University of Washington, Seattle, WA
AIAA-2006-2156
47th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference
14th AIAA/ASME/AHS Adaptive Structures Conference
7th, Newport, Rhode Island, May 1-4, 2006

3.
80%
Probabilistic Approach to Damage Tolerance Design of Aircraft Composite Structures

Kuen Y. Lin; Andrey V. Styuart
Journal of Aircraft 2007
0021-8669 vol.44 no.4 (1309-1317)


4.
77%
2007 Chronological Index

. .
Journal of Aircraft 2007
0021-8669 vol.44 no.6 (2103-2110)


5.
77%
Design and Evaluation of Composite Fuselage Panels Subjected to Combined Loading Conditions

Damodar Ambur; Marshall Rouse
Journal of Aircraft 2005
0021-8669 vol.42 no.4 (1037-1045)


6.
77%
Correction response surface design of stiffened composite panel with a crack

Roberto Vitali and Bhavani V. Sankar (Florida, Univ., Gainesville)
AIAA-1999-1313
AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference and Exhibit, 40th, AIAA/ASME/AHS Adaptive Structures Forum and AIAA Forum on Non-Deterministic Approaches, St. Louis, MO, Apr. 12-15, 1999

7.
77%
Design and evaluation of composite fuselage panels subjected to combined loading conditions

Damodar R. Ambur and Marshall Rouse (NASA, Langley Research Center, Hampton, VA)
AIAA-1997-1303
AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference and Exhibit, 38th, and AIAA/ASME/AHS Adaptive Structures Forum, Kissimmee, FL, Apr. 7-10, 1997, Collection of Technical Papers, Pt. 4 (A97-24112 05-39)