Load of the Reaction ZPL-20 Cannon 20 mm on L-159 ALCA Airplane Stability

Result code in IS VaVaI

<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F60162694%3AG43__%2F12%3A00477331" target="_blank" >RIV/60162694:G43__/12:00477331 - isvavai.cz</a>

Result on the web

<a href="http://vavtest.unob.cz/registr" target="_blank" >http://vavtest.unob.cz/registr</a>

DOI - Digital Object Identifier

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Result language

angličtina

Original language name

Load of the Reaction ZPL-20 Cannon 20 mm on L-159 ALCA Airplane Stability

Original language description

The paper deals with the flow over the L-159 ALCA aircraft airfoils in subsonic regime. Authors have analyzed and assessed the effects of external loads on the aircraft structure during fire. In addition, the impact of the airborne cannon fire on the aircraft stability has been examined. Next, the results of calculations have been analyzed and changes in armament have been proposed. In proposing changes, safe use of cannon in combat has been considered. Moreover, changes also pertained to the aircraft tactical employment mainly at low speeds.

Czech name

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Czech description

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Type

J_x - Unclassified - Peer-reviewed scientific article (Jimp, Jsc and Jost)

CEP classification

KA - Militarism

OECD FORD branch

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Project

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Continuities

I - Institucionalni podpora na dlouhodoby koncepcni rozvoj vyzkumne organizace

Publication year

2012

Confidentiality

S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů

Name of the periodical

American International Journal of Contemporary Research

ISSN

2162-139X

e-ISSN

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Volume of the periodical

Vol. 2

Issue of the periodical within the volume

No. 9

Country of publishing house

CZ - CZECH REPUBLIC

Number of pages

10

Pages from-to

38 - 47

UT code for WoS article

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EID of the result in the Scopus database

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