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Siemens: Femap

(2758 members)
forum1234 - Professional forum and technical support for engineers for Siemens: Femap. Includes problem solving collaboration tools.

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 nlgyro (Aeronautics)
3 replies
(18 Oct 20)
20 Oct 20

plotting nodal stresses

 pbalasu (Aerospace)
1 replies
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16 Oct 20

Coefficient of friction for bolt loads

 RTel (Aerospace)
0 replies
(12 Oct 20)
12 Oct 20

Composite modelling using solid laminates (PCOMPS)

 jonny1230 (Materials)
5 replies
(22 Sep 20)
30 Sep 20

Reaction forces on Cylindrical Composite Tube

 jonny1230 (Materials)
5 replies
(28 Sep 20)
30 Sep 20

Applying Torsion to Composite Cylinder - Very high shear modulus

 BlasMolero (Mechanical)
0 replies
(15 Sep 20)
15 Sep 20

Frequency Response (SOL111) with BOLT Preload and Contact using FEMAP V2020.2 and Simcenter Nastran
2

 MegaStructures (Structural)
12 replies
(3 Sep 20)
5 Sep 20

Local Mesh Refinement and Mesh Convergence under Solid Surface

 ThomasH (Structural)
2 replies
(3 Sep 20)
3 Sep 20

How to cancel the message window in non-linear analysis

 rbas85 (Structural)
3 replies
(31 Aug 20)
3 Sep 20

How to get the centroid of all elements of a group in VB.NET

 CDH007 (Mechanical)
2 replies
(20 Aug 20)
21 Aug 20

Naming of Analysis File in FEMAP Using Local Solver?

 K.O. (Aeronautics)
3 replies
(5 Aug 20)
6 Aug 20

Asking for help for a FLUTTER analysis

 jonny1230 (Materials)
11 replies
(31 Jul 20)
4 Aug 20

How to Output Results for Each Increment From Group in FEMAP

 guilhermemd11 (Aeronautics)
0 replies
(3 Aug 20)
3 Aug 20

FATAL MESSAGE 5266 - TOO MUCH DATA ON TRIM OR AELINK BULK DATA ENTRIES

 MegaStructures (Structural)
2 replies
(27 Jul 20)
27 Jul 20

User Warning Message 4690 (CNTGAPERR) - FEMAP/NASTRAN

 RMM1979 (Aeronautics)
1 replies
(27 Jul 20)
27 Jul 20

Easy way to edit output legends

 NoirSheh (Aerospace)
3 replies
(22 Jul 20)
24 Jul 20

Thermal Stress Analysis Steps

 MegaStructures (Structural)
7 replies
(3 Jul 20)
8 Jul 20

Bolt Shell to Solid

 SuG89 (Structural)
2 replies
(4 Jul 20)
5 Jul 20

MSTAB command in Femap
2

 MegaStructures (Structural)
7 replies
(5 Jun 20)
25 Jun 20

Applying Area Loads to Beam Model

 Mat_Aero (Aerospace)
3 replies
(22 Jun 20)
22 Jun 20

Femap 6060.Laminate Max. Failure Index calculation

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