Blank Cover Image

Free Flexural Vibrations of Integrally-Stiffened and/or Stepped-Thickness Rectangular Plates or Panels with a Central Plate Stiffener

Author(s):
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.:
2007
Pub. Year:
2007
No.:
2007-2113
Paper no.:
AIAA Paper 2007-2113
Pub. info.:
Reston, Va.: American Institute of Aeronautics and Astronautics
ISSN:
10877215
Language:
English
Call no.:
A07400/200707 [CD-ROM 2007 Disc 7]
Type:
Technical Paper

Similar Items:

1 Technical Paper Effects of Central and Non-Central Plate Stiffener on Free Vibrations Response of Integrally-Stiffened and/or Stepped-Thickness Plates or Panels

U. Yuceoglu, Ö. Güvendik, N. Gemalmayan, O. Sunar

American Institute of Aeronautics and Astronautics
7 Technical Paper Free Vibration Characteristics of Composite Shallow Circular Cylindrical Shells or Panels with a Non-Central Single Lap Joint

Yuceoglu, U., Ozerciyes, V.

American Institute of Aeronautics and Astronautics
2 Technical Paper Free Vibrations Analysis of Integrally-Stiffened and/or Stepped-Thickness Plates or Panels with Two Side Stiffeners

U. Yuceoglu, J. Javanshir, S. Eyi

American Institute of Aeronautics and Astronautics
8 Technical Paper Free Non-Axisymmetric Vibrations of Composite Full Cylindrical Shells with a Bonded Non-Central (or Eccentric) Single Lap Joint

Yuceoglu, U., Ozerciyes, V.

American Institute of Aeronautics and Astronautics
3 Technical Paper Sudden drop phenomena in natural frequencies of partially-stiffened, stepped-thickness, composite plates or panels

Yuceoglu, U., Ozerciyes, V.

American Institute of Aeronautics and Astronautics
9 Technical Paper Free Vibrations of Composite Shallow Circular Cylindrical Shell Panels with a Bonded Single Lap Joint

Yuceoglu,U., Ozerciyes,V.

American Institute of Aeronautics and Astronautics
4 Technical Paper Free Vibrations of Composite Shallow Circular Cylindrical Shell Panels Stiffened by A Bonded-Non-Central Shell Strip

Ozerciyes, V., Yuceoglu, U.

American Institute of Aeronautics and Astronautics
10 Technical Paper Free In-plane Vibration of Rectangular Plates

Wang,G., Wereley,N.

American Institute of Aeronautics and Astronautics
5 Technical Paper Free Vibrations of Centrally Bonded Symmetric Lap Joint (or Symmetric Doubler Joint) With a Gap in Mindlin Plates or Panels

O. Guvendik, U. Yuceoglu

American Institute of Aeronautics and Astronautics
11 Technical Paper Free Vibrations of Composite Mindlin Plates with a Symmetric Lap (or Doubler) Joint

Yuceoglu, U., Guvendik, O., Ozerciyes, V.

American Institute of Aeronautics and Astronautics
6 Technical Paper Free Flexural (or Bending) Vibrations of Composite Mindlin Base Plates or Panels with Two Bonded Stiffening Plate Strips

Yuceoglu, Umur, Javanshir, Jaber, Güvendik, Özen

American Institute of Aeronautics and Astronautics
12 Conference Proceedings Free Flexural (or Bending) Vibrations of Orthotropic Composite Mindlin Plates With a Bonded Non-Central (or Eccentric) Lap Joint

U. Yuceoglu, ÁE Güvendik, V. Özerciyes

American Society of Mechanical Engineers
1
 
2
 
3
 
4
 
5
 
6
 
7
 
8
 
9
 
10
 
11
 
12