Pascal and Francis Bibliographic Databases

Help

Search results

Your search

kw.\*:("ENTREE AIR")

Document Type [dt]

A-Z Z-A Frequency ↓ Frequency ↑
Export in CSV

Publication Year[py]

A-Z Z-A Frequency ↓ Frequency ↑
Export in CSV

Discipline (document) [di]

A-Z Z-A Frequency ↓ Frequency ↑
Export in CSV

Language

A-Z Z-A Frequency ↓ Frequency ↑
Export in CSV

Author Country

A-Z Z-A Frequency ↓ Frequency ↑
Export in CSV

Results 1 to 25 of 67

  • Page / 3
Export

Selection :

  • and

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

EFFECT OF FOREBODY SHAPE AND SHIELDING TECHNIQUE ON 2-D SUPERSONIC INLET PERFORMANCE.SURBER LE.1975; IN: AM. INST. AERONAUT. ASTRONAUT.-SOC. AUTOMOT. ENG. PROPUL. CONF. 11; ANAHEIM, CALIF.; 1975; NEW YORK; A.I.A.A.; DA. 1975; VOL. 1183; PP. 1-19; BIBL. 8 REF.Conference Paper

UNIQUE APPLICATIONS OF THE METHOD OF CHARACTERISTICS TO INLET AND NOZZLE DESIGN PROBLEMS.HENNE PA.1975; IN: AM. INST. AERONAUT. ASTRONAUT.-SOC. AUTOMOT. ENG. PROPUL. CONF. 11; ANAHEIM, CALIF.; 1975; NEW YORK; A.I.A.A.; DA. 1975; VOL. 1185; PP. 1-9; BIBL. 15 REF.Conference Paper

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

SOME ASPECTS OF FAN NOISE SUPPRESSION USING HIGH MACH NUMBER INLETS.SAVKAR SD; KAZIN SB.1974; IN: AM. INST. AERONAUT. ASTRONAUT. 7TH FLUID PLASMA DYN. CONF.; PALO ALTO, CALIF.; 1974; NEW YORK; A.I.A.A.; DA. 1974; VOL. 554; PP. 1-13; BIBL. 10 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

LOW COST OPTIMIZED PERFORMANCE INLETS FOR RAMJETS.KOETJE EL.1976; IN: STRUCT. STRUCT. DYN. MATER. CONF. 17. PROC.; KING OF PRUSSIA, PA.; 1976; S.L.; AM. INST. AERONAUT. ASTRONAUT.; DA. 1976; PP. 229-233Conference Paper

ESTIMATING MAXIMUM INSTANTANEOUS DISTORTION FROM INLET TOTAL PRESSURE RMS AND PSD MEASUREMENT.MELICK HC JR; YBARRA AH; BENCZE DP et al.1975; IN: AM. INST. AERONAUT. ASTRONAUT.-SOC. AUTOMOT. ENG. PROPUL. CONF. 11; ANAHEIM, CALIF.; 1975; NEW YORK; A.T.A.A.; DA. 1975; VOL. 1213; PP. 1-13; BIBL. 12 REF.Conference Paper

LUTTE CONTRE LES POUSSIERES PRODUITES DANS UNE STATION DE CULBUTAGEKOTELEVSKIJ PA; KOSENKO KM; KUZNETSOV YU F et al.1973; BEZOPASM. TRUDA PROMYSHL.; S.S.S.R.; DA. 1973; NO 3; PP. 18-19Serial Issue

LE RECHAUFFAGE DE L'AIR DANS LES PUITS CUVELESANDREICHEV AN.1972; BEZOPASN. TRUDA PROMYSHL.; S.S.S.R.; DA. 1972; NO 9; PP. 42-43Serial Issue

INSTALLATION CAUSED FLOW DISTORTION AND ITS EFFECT ON NOISE FROM A FAN DESIGNED FOR TURBOFAN ENGINES = DISTORTION DE L'ECOULEMENT DU A L'INSTALLATION ET SON EFFET SUR LE BRUIT D'UNE SOUFFLANTE CONCUE POUR TURBOREACTEUR A SOUFFLANTE CANALISEEPOVINELLI FP; DITTMAR JH.sdIN: AIAA 7TH AERODYN. TEST. CONF. PALO ALTO, CALIF., 1972; NEW YORK; AM. INST. AERONAUT. ASTRONAUT.; DA. S.D.; NO 993; PP. 1-10; BIBL. 12 REF.Conference Paper

2.252.489 (A1) (7438741). - 26 NOVEMBRE 1974. DISPOSITIF DE REGLAGE DE L'ENTREE D'AIR POUR DES GROUPES PROPULSEURS D'AVIONS A ASPIRATION D'AIRsdPatent

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

  • Page / 3