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COMPARISON OF TESTING TECHNIQUES FOR ISOLATED AXISYMMETRIC EXHAUST NOZZLES IN TRANSONIC FLOW.

Author
LAUGHREY JA
AIR FORCE FLIGHT DYN. LAB., WRIGHT-PATTERSON AIR FORCE BASE, OHIO
Source
IN: AM. INST. AERONAUT. ASTRONAUT.-SOC. AUTOMOT. ENG. PROPUL. CONF. 11; ANAHEIM, CALIF.; 1975; NEW YORK; A.I.A.A.; DA. 1975; VOL. 1292; PP. 1-11; BIBL. 9 REF.
Document type
Conference Paper
Language
English
Keyword (fr)
TUYERE JET AXISYMETRIQUE ESSAI SOUFFLERIE ECOULEMENT TRANSSONIQUE INTERACTION PAROI
Classification
Pascal
001 Exact sciences and technology / 001B Physics

Discipline
Theoretical physics
Origin
Inist-CNRS
Database
PASCAL
INIST identifier
PASCAL7630135028

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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