Hi,
I'm trying to make a Macro for Drawing Title Block.
I can't applied the following proprieties to my new text (will be the drawing number):
Flip Mode (Horizontal);
Orientation (Vertical).
For the Flip Mode I've tried with this input in the Script:
Dim Tex1Prop As Drawing TextProperties...
Hi mohr,
Thanks a lot for your suggestion..
I've the book: J. H. Argyris, S. Kelsey "Modern Fuselage Analysis and Elastic Aircraft" and it is a great work!! Perfect suitable for digital computer application. Inside this book is cited the work of Dr. Przemienicki "Matrix Analysis of Shell...
Crackman,
thanks a lot for all help.
Grazie davvero per tutto l'aiuto. Conosco la zona di Trieste, ho avuto diversi colleghi e collaboratori della zona. Io non sono mai stato in America, anche se ho collaborato per diversi anni con grandi Aziende americane aeronautiche, a Venezia. Molti miei...
Crackman,
thanks a lot for your post. I know the National Aerospace Library and I agree with you, the staff is excellent under all aspects. I live in Venice (Italy) so for me it is not easy to visit it, but with the support of stuff I obtain a lot of old papers and documents (just for example 2...
Andries,
thanks a lot for your post. I think that Force Method is a very good tool for structural analysis, in particular for "quick look analysis" in aircraft structures. I read a lot of work of Dr. Robinson (in particular The Rank Force Method).
I have all the books that you kindly suggest to...
Thanks a lot for all information, dear crackman.
I'll try to find it in Smithsonian and National Archive as You suggest. I'm interesting about Matrix Force Method applied to aircraft structures.
Please when Your books will be ready kindly contact me I'd like to buy it. I'm intersting in...
Hi,
I'm trying to find the following Paper:
Islinger J. S., "Stress analysis and stress measurement for a swept back wing having ribs parallel to the airstream", McDonnel Aircraft Corp., Report 1127, April 1949.
There is someone who can help me for my research?...
thanks a lot to everybody!!..
Hi,
with reference to I. Taig "Aircraft FEM Notes", and in particular about Rigid Body Movements Check, I don't understand why NASTRAN deck should contain DAMMY (UNIT) LOAD data for each subcase (relative to movement and rotation for each of the 6 D.O.F.).
Thanks to all!!
I made a typing error.
The CORRECT version is:
"I have to show in Installation VIEWs some ASSYs only for reference (PHANTOM LINE TYPE - not included in Bill Of Material)."
Thanks.
Hi,
I have to make some CATIA V5 Drafting VIEWs of an airframe Installation.
I have to show in Installation VIEWs to some ASSYs only for reference (PHANTOM LINE TYPE - not included in Bill Of Material).
Can someone help me to find the best why to do this?.
In V4 I add the ASSY in the V4-SESSION...