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A MODEL FOR THE EVALUATION OF INDUCED ROLLING MOMENTS AND SIDE FORCES IN SLENDER CRUCIFORM CANARD CONFIGURATIONS AT SMALL ANGLES OF INCIDENCE.

Author
GUR I; SHINAR J; ROM J
TECHNION-ISRAEL INST. TECHNOL., HAIFA, ISR.
Source
ISRAEL J. TECHNOL.; ISRAEL; DA. 1976; VOL. 14; NO 1-2; PP. 74-85; BIBL. 18 REF.; (ISR. ANNU. CONF. AVIAT. ASTRONAUT. 18. PROC.; TEL AVIV-HAIFA; 1976)
Document type
Conference Paper
Language
English
Keyword (fr)
CONFIGURATION CANARD AILE AERODYNAMIQUE MODELE MATHEMATIQUE MOMENT ROULIS FORCE AERODYNAMIQUE
Keyword (en)
WING AERODYNAMICS MATHEMATICAL MODELS AERODYNAMIC FORCE
Classification
Pascal
001 Exact sciences and technology / 001B Physics

Discipline
Theoretical physics
Origin
Inist-CNRS
Database
PASCAL
INIST identifier
PASCAL7730112032

Sauf mention contraire ci-dessus, le contenu de cette notice bibliographique peut être utilisé dans le cadre d’une licence CC BY 4.0 Inist-CNRS / Unless otherwise stated above, the content of this bibliographic record may be used under a CC BY 4.0 licence by Inist-CNRS / A menos que se haya señalado antes, el contenido de este registro bibliográfico puede ser utilizado al amparo de una licencia CC BY 4.0 Inist-CNRS

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