DEVELOPPEMENTS NOUVEAUX DANS LE FORGEAGE DES GROSSES PIECES POUR LES MATERIELS AERONAUTIQUESQUINTAA M.1972; METALLURG. CONSTR. MEC.; FR.; DA. 1972; VOL. 104; NO 9; PP. 333-338Serial Issue

THE USE OF A ROTATING ARM FACILITY TO STUDY FLIGHT EFFECTS ON JET NOISE.SMITH W.sdIN: 2ND INT. SYMP. AIR BREATHING ENGINES, PROC.; SHEFFIELD, ENGL.; 1974; LONDON; R. AERONAUT. SOC.; DA. S.D.; PP. (13P.)Conference Paper

A ROTARY ENGINE DEVELOPMENT.HUBBARD G.1976; A.I.A.A. MONOGR.; U.S.A.; DA. 1976; VOL. 21; PP. 47-48Article

APPLYING SURFACE INTEGRITY PRINCIPLES IN JET ENGINE PRODUCTIONBELLOWS G.1972; METALS ENGNG QUART.; U.S.A.; DA. 1972; VOL. 12; NO 4; PP. 55-58; BIBL. 9 REF.Serial Issue

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

AIRCRAFT AND AIRPORT NOISE1972; IN: INT. CONF. NOISE CONTROL ENG. PROC. WASHINGTON, D.C., 1972; S.L.; INST. NOISE CONTROL ENG.; DA. 1972; PP. 319-371; BIBL. DISSEM.Conference Proceedings

CENTRALIZED IN-PLACE PRESSURE CALIBRATION SYSTEM FOR MULTIPLE TURBINE ENGINE AERODYNAMIC PRESSURE MEASUREMENT SYSTEMSBROCK WN.1980; INSTRUMENTATION IN THE AEROSPACE INDUSTRY. ADVANCES IN TEST MEASUREMENT. INTERNATIONAL INSTRUMENTATION SYMPOSIUM. 26/1980/SEATTLE WA; USA; RESEARCH TRIANGLE PARK NC: INSTRUMENT SOCIETY OF AMERICA; DA. 1980; VOL. 1; PP. 353-360Conference Paper

APPLICATIONS OF FLOW DIAGNOSTIC TECHNIQUES TO AERODYNAMIC PROBLEM SOLVING.GEORGE FALVY D.1976; IN: AERODYN. TEST. CONF. 9. PROC.; ARLINGTON, TEX.; 1976; S.L.; AM. INST. AERONAUT. ASTRONAUT.; DA. 1976; PP. 246-260; BIBL. 4 REF.Conference Paper

PREPARATION DES COMBUSTIBLES SOLVANTS AROMATIQUES ET NON AROMATIQUES POUR LES MOTEURS A REACTION A PARTIR DE LA FRACTION CARBUREACTEUR DU PETROLE EN UTILISANT L'EXTRACTION AVEC DES SOLVANTS MIXTESORESKOVIC B; KNEZEVIC E; PROTIC G et al.1974; NAFTA; JUGOSL.; DA. 1974; VOL. 25; NO 9; PP. 479-485; ABS. ANGL. RUSSE; BIBL. 10 REF.Article

AN ADVANCED TURBINE FLOWMETER SYSTEM WITH DENSITY COMPENSATION.STUART DE.1974; IN: FLOW. MEAS. CONTROL IN SCI. IND. SYMP. 1. PROC.; PITTSBURGH, PA.; 1971; PITTSBURGH; INSTRUM SOC. AM.; DA. 1974; PP. 695-700; BIBL. 4 REF.Conference Paper

EFFECT ON SUPERSONIC JET NOISE OF NOZZLE PLENUM PRESSURE FLUCTUATIONS = EFFET DES FLUCTUATIONS DE PRESSION GENERATRICE D'UNE TUYERE SUR LE BRUIT D'UN MOTEUR A REACTION SUPERSONIQUEKUSHIDA R; RUPE J.1972; A.A.I.A.A.J., NEW YORK; U.S.A.; DA. 1972; VOL. 10; NO 7; PP. 946-948; BIBL. 6 REF.Serial Issue

SILENCIEUX ET INVERSEURS DE POUSSEE POUR REACTEURSJUMELLE ML.1972; INGRS DE L'AUTOM.; FR.; DA. 1972; NO 6-7; PP. 369-382; BIBL. 2 REF.Serial Issue

PROPRIETES DIELECTRIQUES DES CARBURANTS POUR MOTEURS A REACTIONSNITSEROV YU V; ATANOV YU A; PRISYAZHNYJ SV et al.1972; KHIM. TEKHNOL. TOPL. MASEL; S.S.S.R.; DA. 1972; VOL. 17; NO 7; PP. 40-43; BIBL. 15 REF.Serial Issue

CHEMITOLOGIC RELIABILITY OF JET TECHNOLOGYPISKUNOV VA; PAPOK KK; ZRELOV VN et al.1978; KHIM. TEKHNOL. TOPL. MASEL; SUN; DA. 1978; NO 11; PP. 4-8; BIBL. 7 REF.Article

AIRCRAFT/ENGINE JET NOISE CONTROL. A SURVEY = REDUCTION DU BRUIT DES MOTEURS A REACTION D'AVION. REVUESTRINGAS EJ; MANI R.1974; IN: AIAA 6TH AIRCR. DES. FLIGHT TEST OPER. MEET.; LOS ANGELES; 1974; NEW YORK; AIAA; DA. 1974; VOL. 947; PP. 1-24; BIBL. 12 REF.Conference Paper

NOISE: A TRIUMPH OF IGNORANCE = LE BRUIT: TRIOMPHE DE L'IGNORANCEKOLK FW.1972; ASTRONAUT. AND AERONAUT.; U.S.A.; DA. 1972; VOL. 10; NO 10; PP. 20-31 (11 P.)Serial Issue

DESIGNING FOR NOISE REDUCTIONSCHAIRER GS; GEREND RP.sdIN: SYMP. IMPACT ECON. DESIGN OPER. QUIETER AIRE. PROC.; LONDON; 1975; LONDON; R. AERONAUT. SOC.; DA. S.D.; PP. (24 P.); BIBL. 49 REF.Conference Paper

GROUND NOISE SUPPRESSORS FOR AIRCRAFT ENGINE OPERATION = SUPPRESSEURS DU BRUIT AU SOL POUR LE FONCTIONNEMENT DES MOTEURS D'AVIONMILLER CJ.1975; IN: AM. INST. AERONAUT. ASTRONAUT.-SOC. AUTOMOT. ENG. PROPUL. CONF. 11; ANAHEIM, CALIF.; 1975; NEW YORK; A.I.A.A.; DA. 1975; VOL. 1327; PP. 1-5Conference Paper

STATUS OF THE JT8D REFAN NOISE REDUCTION PROGRAMKESTER JD.1975; NOISE CONTROL ENGNG; U.S.A.; DA. 1975; VOL. 5; NO 2; PP. 75-79Article

DIE ANWENDUNG VON TITANGUSSTEILEN IM MRCA TRIEBWERK RB 199 ZUR HERSTELLUNG EINES KOMPLEXEN ZWISCHENGEHAEUSES = UTILISATION DE PIECES COULEES EN TITANE DANS LE REACTEUR MRCA-RB 199 POUR LA FABRICATION DE CARTERS INTERMEDIAIRES COMPLEXESHANSEN WG.1975; Z. WERKST.-TECH.; DTSCH.; DA. 1975; VOL. 6; NO 11; PP. 361-367; ABS. ANGLArticle

JET ENGINE SOOT EMISSION MEASURED AT ALTITUDEROSEN JM; GREEGOR R.1974; J. AIRCR.; U.S.A.; DA. 1974; VOL. 11; NO 4; PP. 243-245; BIBL. 5 REF.Article

TITANIUM JET ENGINE PARTS JOINED WITH PLASMA ARC = SOUDAGE AU PLASMA D'ELEMENTS EN TITANE DE MOTEURS A REACTION1974; METAL PROGR.; U.S.A.; DA. 1974; VOL. 106; NO 2; PP. 79Article

EVALUATING THE RISK TO SOCIETY FROM THE SST: SOME THOUGHTS OCCASIONED BY THE AAS REPORTPITTOCK AB.1972; SEARCH; AUSTRAL.; DA. 1972; VOL. 3; NO 8; PP. 285-289; BIBL. 14 REF.Serial Issue

LIFTING FAN NOISE STUDIES WITH SUPERIMPOSED CROSS FLOWS = ETUDE DU BRUIT PROVENANT DE SOUFFLANTES DE SUSTENTATION EN PRESENCE D'ECOULEMENTS TRANSVERSAUX SUPERPOSESKRISHNAPPA G.1972; J. AIRCR.; U.S.A.; DA. 1972; VOL. 9; NO 10; PP. 719-725; BIBL. 6 REF.Serial Issue

REPLY TO FOUR CRITICISMS OF THE ACADEMY REPORT ATMOSPHERIC EFFECTS OF SUPERSONIC AIRCRAFTPRIESTLEY CHB.1972; SEARCH; AUSTRAL.; DA. 1972; VOL. 3; NO 8; PP. 298-301Serial Issue