Geodesic
Software development for subsonic aircraft’s unsteady longitudinal stability derivatives calculation
Theoretical and applied mechanics, Tome 32 (2005) no. 4.

Voir la notice de l'article provenant de la source eLibrary of Mathematical Institute of the Serbian Academy of Sciences and Arts

Subsonic general configuration aircrafts’ unsteady longitudinal aerodynamic stability derivatives can be estimated using finite element methodology based on the Doublet Lattice Method (DLM), the Slender Body Theory (SBT) and the Method of Images (MI). Applying this methodology, software DERIV is developed. The obtained results from DERIV are compared to NASTRAN examples HA21A and HA75H. A good agreement is achieved.
Keywords: unsteady aerodynamics, stability derivatives 
@article{TAM_2005_32_4_a1,
     author = {Nikola Mari\v{c}i\'c},
     title = {Software development for subsonic aircraft{\textquoteright}s unsteady longitudinal stability derivatives calculation},
     journal = {Theoretical and applied mechanics},
     pages = {319 - 340},
     publisher = {mathdoc},
     volume = {32},
     number = {4},
     year = {2005},
     url = {http://geodesic.mathdoc.fr/item/TAM_2005_32_4_a1/}
}
TY  - JOUR
AU  - Nikola Maričić
TI  - Software development for subsonic aircraft’s unsteady longitudinal stability derivatives calculation
JO  - Theoretical and applied mechanics
PY  - 2005
SP  - 319 
EP  -  340
VL  - 32
IS  - 4
PB  - mathdoc
UR  - http://geodesic.mathdoc.fr/item/TAM_2005_32_4_a1/
ID  - TAM_2005_32_4_a1
ER  - 
%0 Journal Article
%A Nikola Maričić
%T Software development for subsonic aircraft’s unsteady longitudinal stability derivatives calculation
%J Theoretical and applied mechanics
%D 2005
%P 319 - 340
%V 32
%N 4
%I mathdoc
%U http://geodesic.mathdoc.fr/item/TAM_2005_32_4_a1/
%F TAM_2005_32_4_a1
Nikola Maričić. Software development for subsonic aircraft’s unsteady longitudinal stability derivatives calculation. Theoretical and applied mechanics, Tome 32 (2005) no. 4. http://geodesic.mathdoc.fr/item/TAM_2005_32_4_a1/