ADVANCED SUPERSONIC INLET TECHNOLOGY = TECHNOLOGIE DES ENTREES D'AIR SUPERSONIQUES DE CONCEPTION AVANCEESORENSEN NE; SMELTZER DB; LATHAM EA et al.1973; J. AIRCR.; U.S.A.; DA. 1973; VOL. 10; NO 5; PP. 278-282; BIBL. 13 REF.Serial Issue

SUBSONIC FLOW INTO A DOWNSTREAM FACING INLET.KEITH TG JR.1974; J. AIRCR.; U.S.A.; DA. 1974; VOL. 11; NO 4; PP. 251-252; BIBL. 1 REF.Article

ESSAIS D'ENTREES D'AIR EN SOUFFLERIE.LAVERRE J; BAZIN M; LEDY JP et al.1974; IN: 9TH CONGR. INT. COUNC. AERONAUT. SCI. PROC.; HAIFA; 1974; JERUSALEM; WEIZMANN SCI. PRESS ISR.; DA. 1974; VOL. 2; PP. 677-690; ABS. ANGL.; BIBL. 10 REF.Conference Paper

DESIGN FOR ELIMINATION OF VORTEX FORMATION AT INLETS.ZIELINSKI PB.1974; IN: ASCE NATL. MEET. WATER RES. ENG. PREPR.; LOS ANGELES, CALIF.; 1974; S.L.; DA. 1974; VOL. 2160; PP. (20P.); BIBL. 14 REF.Conference Paper

THE EFFECT OF INLET DISTORTION ON THE PERFORMANCE AND STABILITY OF THE LOW-SPEED SPOOL OF A TURBOFAN ENGINE.KORN JA.1974; IN: AM. INST. AERONAUT. ASTRONAUT. 12TH AEROSP. SCI. MEET.; WASHINGTON; 1974; NEW YORK; A.I.A.A.; DA. 1974; VOL. 234; PP. 1-11Conference Paper

AN EXPERIMENTAL INVESTIGATION OF GROUND VORTEX FORMATION DURING REVERSE ENGINE OPERATION.MOTYCKA DL; WALTER WA.1975; IN: AM. INST. AERONAUT. ASTRONAUT.-SOC. AUTOMOT. ENG. PROPUL. CONF. 11; ANAHEIM, CALIF.; 1975; NEW YORK; A.I.A.A.; DA. 1975; VOL. 1322; PP. 1-4; BIBL. 2 REF.Conference Paper

CALCULATION OF TRANSONIC FLOW AROUND AXISYMMETRIC INLETS.ARLINGER BG.1975; A.I.A.A. J., NEW YORK; U.S.A.; DA. 1975; VOL. 13; NO 12; PP. 1614-1621; BIBL. 12 REF.Article

PROPULSION CHARACTERISTICS AFFECTING THE AERODYNAMIC PERFORMANCE OF AN EXTERNALLY BLOWN FLAP TRANSPORT MODEL.HOAD DR.1975; IN: AM. INST. AERONAUT. ASTRONAUT.-SOC. AUTOMOT. ENG. PROPUL. CONF. 11; ANAHEIM, CALIF.; 1975; NEW YORK; A.I.A.A.; DA. 1975; VOL. 1218; PP. 1-4; H.T. 3; BIBL. 14 REF.Conference Paper

DYNAMIC FLOW DISTORTION IN SUBSONIC AIR INLETS.JONES JR; DOUGLASS WM.sdIN: 2ND INT. SYMP. AIR BREATHING ENGINES. PROC.; SHEFFIELD, ENGL.; 1974; LONDON; R. AERONAUT. SOC.; DA. S.D.; PP. (13P.); BIBL. 4 REF.Conference Paper

INVESTIGATION OF SEPARATED FLOW OVER BODIES OF REVOLUTION IN SUPERSONIC INTAKE DUCTS.ZAKHAROV NN.sdIN: 2ND INT. SYMP. AIR BREATHING ENGINES. PROC.; SHEFFIELD, ENGL.; 1974; LONDON; R. AERONAUT. SOC.; DA. S.D.; PP. (12P.); BIBL. 5 REF.Conference Paper

PRESSURE MEASUREMENTS FOR ESTABLISHING INLET/ENGINE COMPATIBILITY = MESURES DE PRESSION POUR ETABLIR LA COMPATIBILITE ADMISSION/MOTEUREGGERS WC.1974; I.S.A. TRANS.; U.S.A.; DA. 1974; VOL. 13; NO 3; PP. 226-231; BIBL. 4 REF.Article

CONTROL OF SHOCK-WAVE BOUNDARY-LAYER INTERACTIONS BY BLEED IN SUPERSONIC MIXED COMPRESSION INLETS.FUKUDA MK; ROSHOTKO E; HINGST WR et al.1975; IN: AM. INST. AERONAUT. ASTRONAUT.-SOC. AUTOMOT. ENG. PROPUL. CONF. 11; ANAHEIM, CALIF.; 1975; NEW YORK; A.I.A.A.; DA. 1975; VOL. 1182; PP. 1-8; BIBL. 14 REF.Conference Paper

SUR L'ECOULEMENT AUTOUR D'UNE PRISE D'AIR.WERLE H; GALLON M.1975; RECH. AEROSPAT.; FR.; DA. 1975; NO 2; PP. 81-92; ABS. ANGL.; BIBL. 23 REF.Article

F-12 INLET DEVELOPMENTCAMPBELL DH.1974; S.A.E. TRANS.; U.S.A.; DA. 1974; VOL. 83; NO PART. 3; PP. 2832-2840; BIBL. 5REF.Article

PROBLEMES D'INTERACTIONS ENTRE LA PRISE D'AIR ET L'AVION.LEYNAERT J.1974; CHATILLON; OFF. NATL. ETUD. RECH. AEROSP.; DA. 1974; PP. 1-11; ABS. ANGL.; BIBL. 25 REF.; (REUN. AGARD INTERFERENCE ENTRE CELL. PROPUL.; ROME; 1974)Conference Paper

PREDICTION OF INLET DUCT OVERPRESSURES RESULTING FROM ENGINE SURGE = PREVISION DES SURPRESSIONS DE CONDUITES D'ENTREE D'AIR PROVENANT D'UN ENGORGEMENT DU MOTEURMARSHALL FL.1973; J. AIRCR.; U.S.A.; DA. 1973; VOL. 10; NO 5; PP. 274-278; BIBL. 11 REF.Serial Issue

SOLUTION DES PROBLEMES D'INGENIERIE DES EQUIPEMENTS DE SURFACE DES PUITS D'ENTREE D'AIR DANS LES REGIONS A PERGELISOLCHESKIS IS.1972; SHAKHTNOE STROITEL.; S.S.S.R.; DA. 1972; NO 7; PP. 13-16Serial Issue

A NOVEL CONCEPT FOR SUBSONIC INLET BOUNDARY-LAYER CONTROL.MILLER BA.1977; J. AIRCR.; U.S.A.; DA. 1977; VOL. 14; NO 4; PP. 403-404; BIBL. 6 REF.Article

COMPARISON OF CONVENTIONAL AND FORCE-BASED DISTORTION INDEX MEASUREMENTS.SAJBEN M; CHEN CP; KROUTIL JC et al.1976; A.I.A.A. J., NEW YORK; U.S.A.; DA. 1976; VOL. 14; NO 10; PP. 1500-1501; BIBL. 4 REF.Article

INVESTIGATION OF THE USE OF HOLOGRAPHY IN STUDYING SUPERSONIC FLOW IN INLETS.SPRING WV III; RAGSDALE WC.1974; PROGR. ASTRONAUT. AERONAUT.; U.S.A.; DA. 1974; VOL. 34; PP. 95-106; BIBL. 9 REF.Article

OPERATING EXPERIENCE WITH GAS TURBINE CONTAINER SHIPSO'HARE TLR; HOLBURN JG.1973; INST. MAR. ENGRS, TRANS.; G.B.; DA. 1973; VOL. 85; NO 1; PP. 1-24Serial Issue

BEITRAG ZUM PROBLEM DES EINSAUGENS VON FREMDKOERPERN IN TRIEBWERKSEINLAEUFE = CONTRIBUTION A L'ETUDE DU PROBLEME DE L'ASPIRATION DE CORPS ETRANGERS DANS L'ENTREE DES PROPULSEURSPFLUGSHAUPT H.sdIN: 5. JAHRESTAG. DTSCH. GES. LUFT RAUMFAHRT; BERLIN; 1972; S.L.; DA. S.D.; PP. 1-34; H.T. 20; BIBL. 1 P. 1/2Conference Paper

SELECTION GUIDE TO BOILER INSTRUMENTATIONCHO CH.1981; HYDROCARBON PROCESS.; ISSN 0018-8190; USA; DA. 1981; VOL. 60; NO 8; PP. 82-88Article

CONCORDE'S OLYMPUS 593. THE BRITISH CENTREPIECE AT THE PEKING EXHIBITION = L'OLYMPUS 593 DE CONCORDE. LA PIECE CENTRALE BRITANNIQUE A L'EXPOSITION DE PEKIN1973; AIRCR. ENGNG; G.B.; DA. 1973; VOL. 45; NO 3; PP. 6-8Serial Issue

EXPERIMENTALLY DETERMINED AEROACOUSTIC PERFORMANCE AND CONTROL OF SEVERAL SONIC INLETSMILLER BA.1975; IN: AM. INST. AERONAUT. ASTRONAUT.-SOC. AUTOMOT. ENG. PROPUL. CONF. II; ANAHEIM, CALIF.; 1975; NEW YORK; A.I.A.A.; DA. 1975; VOL. 1184; PP. 1-15; BIBL. 18 REF.Conference Paper