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COMMENT LOCALISER LES PRISES D'AIR EXTERIEUR DANS UN ENVIRONNEMENT CONTAMINETROJANOWSKI T.1973; BULL. INST. INTERNATION. FROID, ANNEXE; FR.; DA. 1973; NO 2; PP. 129-138; ABS. ANGL.; BIBL. 9 REF.Article

ETUDE DU PROCESSUS D'ENTREE D'UN FLUX D'AIR DANS UNE PRISE D'AIR AVEC UN ECRAN PAR LA METHODE DE L'ANALOGIE ELECTROHYDRODYNAMIQUEGRISHIN IA; IVANNIKOV VF; NESTEROV ED et al.1977; IZVEST. VYSSH. UCHEBN. ZAVED., AVIAC. TEKH.; S.S.S.R.; DA. 1977; VOL. 20; NO 1; PP. 134-137; BIBL. 1 REF.Article

Allowing for real ear venting effects when selecting the coupler gain of hearing aidsDILLON, H.Ear and hearing. 1991, Vol 12, Num 6, pp 406-416, issn 0196-0202Article

Effect of adding oxygen to the intake air on a dual-fuel engine performance, emissions, and knock tendencyABDELAAL, Mohsen M; RABEE, Basem A; HEGAB, Abdelrahman H et al.Energy (Oxford). 2013, Vol 61, pp 612-620, issn 0360-5442, 9 p.Article

Etude expérimentale de l'écoulement dans le modèle d'une prise d'air convergente à parois planesGUTOV, B. I; ZATOLOKA, V. V.Prikladnaâ mehanika i tehničeskaâ fizika. 1985, Num 6, pp 62-68, issn 0869-5032Article

CALCUL DE DISPOSITIFS DE PRISE D'AIR DANS UNE COUCHE LIMITEKALUGIN VT; KLEBANOVA TV; KOZLOV YU I et al.1979; IZVEST. VYSSH. UCHEBN. ZAVED., AVIAC. TEKH.; SUN; DA. 1979; VOL. 22; NO 1; PP. 93-96; BIBL. 6 REF.Article

ETUDE THEORIQUE ET EXPERIMENTALE D'UN STATOREACTEUR A COMBUSTION MIXTE (DOMAINE DE VOL MACH 3,5/7CONTENSOU P; MARGUET R; HUET C et al.sdIN: 8TH CONGR. INT. COUNC. AERONAUT. SCI.; AMSTERDAM; 1972; NEW YORK; AM. INST. AERONAUT. ASTRONAUT.; DA. S.D.; VOL. 24; PP. 1-15; ABS. ANGL.; BIBL. 12 REF.Conference Paper

Determination of the Terminal Shock in Two-Dimensional Supersonic InletsHONGJUN RAN; DENNEY, Russell; MAVRIS, Dimitri N et al.Journal of aircraft. 2012, Vol 49, Num 5, pp 1532-1535, issn 0021-8669, 4 p.Article

Influence of EGR and oxygen-enriched air on diesel engine NO―Smoke emission and combustion characteristicWEI ZHANG; ZHAOHUI CHEN; WEIDONG LI et al.Applied energy. 2013, Vol 107, pp 304-314, issn 0306-2619, 11 p.Article

Test Technique for the Measurement of Intake Drag of Air-Breathing VehiclesMATHUR, N. B; AHMED, Sajeer.Journal of aircraft. 2012, Vol 49, Num 6, pp 2092-2095, issn 0021-8669, 4 p.Article

Turbine inlet air coolingSTEWART, W. E.ASHRAE journal. 1998, Vol 40, Num 9, pp 32-37, issn 0001-2491, 4 p.Article

A simplified irreversible Otto engine model with fluctuations in the combustion heatROCHA-MARTINEZ, J. A; NAVARRETE -GONZALEZ, T. D; PAVIA-MILLER, C. G et al.International journal of ambient energy. 2006, Vol 27, Num 4, pp 181-192, issn 0143-0750, 12 p.Article

Robust design of gas and liquid micropumpsRICHTER, M; LINNEMANN, R; WOIAS, P et al.Sensors and actuators. A, Physical. 1998, Vol 68, Num 1-3, pp 480-486, issn 0924-4247Conference Paper

Understanding and countering the swirl in S-ducts: tests on the sensitivity of swirl to fencesSEDDON, J.Aeronautical Journal. 1984, Vol 88, Num 874, pp 117-127, issn 0001-9240Article

METHODS FOR SOLVING EULER'S EQUATIONS FOR AIRFOIL AND INTAKE FLOWEBERLE A.1982; CONFERENCE ON NUMERICAL METHODS IN FLUID MECHANICS. 4/1981/PARIS; DEU; BRAUNSCHWEIG; WIESBADEN: F. VIEWEG; DA. 1982; PP. 77-86; BIBL. 6 REF.Conference Paper

ON SOUND CHARACTERISTICS OF AIR OUTLETS AND INLETS = CARACTERISTIQUES ACOUSTIQUES DES SORTIES ET DES ENTREES D'AIRITAMOTO M.1975; IN: INTER-NOISE 75. INT. CONF. NOISE CONTROL ENG. PROC.; SENDAI; 1975; SENDAI; TOHOKU UNIV.; DA. 1975; PP. 671-674Conference Paper

The influence of several design features of the inlet and outlet of an axial fan on its characteristicsTUPOV, V. B.Thermal engineering. 1997, Vol 44, Num 11, pp 950-955, issn 0040-6015Article

Strategy for developing air-breathing aerospace planesMEHTA, U. B.Journal of aircraft. 1996, Vol 33, Num 2, pp 377-385, issn 0021-8669Conference Paper

Computational inlet-fairing effects and plume characterization on a hypersonic powered modelHUEBNER, L. D.Journal of aircraft. 1995, Vol 32, Num 6, pp 1240-1245, issn 0021-8669Conference Paper

Static pressure distribution in the inlet of a helicopter turbine compressorVAN DER WALT, J. P; NURICK, A.Journal of aircraft. 1994, Vol 31, Num 6, pp 1411-1413, issn 0021-8669Article

A new approach for the design of hypersonic scramjet inletsOM PRAKASH RAJ, N; VENKATASUBBAIAH, K.Physics of fluids (1994). 2012, Vol 24, Num 8, issn 1070-6631, 0866103.1-086103.15Article

Operational performance of inlet barrier filters for rotorcraftBOJDO, N; FILIPPONE, A.Aeronautical Journal. 2012, Vol 116, Num 1182, pp 847-869, issn 0001-9240, 23 p.Article

Designing dedicated outdoor Air systemsMUMMA, Stanley A.ASHRAE journal. 2001, Vol 43, Num 5, pp 28-31, issn 0001-2491Article

Calculation of the supersonic perfect gas flow in an hypersonic air-intakeBASHKIN, V. A; EGOROV, I. V; IVANOV, D. V et al.Fluid dynamics. 1996, Vol 31, Num 5, pp 785-792, issn 0015-4628Article

New approach to low-noise air intake system developmentNISHIO, Y; KOHAMA, T; KURODA, O et al.SAE transactions. 1991, Vol 100, Num 6, pp 1388-1400, issn 0096-736XArticle

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