QUIETING THE DIESEL WITH STRUCTURAL CHANGETIEDE DD; KABELE DF.1972; AUTOMOT. ENGNG; U.S.A.; DA. 1972; VOL. 80; NO 12; PP. 31-33; BIBL. 5 REF.Serial Issue

INTERNATIONAL REGULATION OF AIRCRAFT NOISEMEYNELL BW.1971; S.A.E. TRANS.; U.S.A.; DA. 1971; VOL. 80; PART 2; PP. 1411-1415; BIBL. 4 REF.Serial Issue

FORWARD FLIGHT EFFECTS ON MIXER NOZZLE DESIGN AND NOISE CONSIDERATIONS FOR STOL EXTERNALLY BLOWN FLAP SYSTEMS = EFFETS DU VOL EN TRANSLATION SUR LA CONCEPTION D'UNE TUYERE A MELANGEUR ET CONSIDERATIONS DE BRUIT POUR LES SYSTEMES DE VOLETS SOUFFLES DE L'EXTERIEUR D'AVION ADACVON GLAHN U; SEKAS N; GROESBECK D et al.sdIN: AIAA 4TH AIRCR. DES. FLIGHT TEST OPER. MEET. LOS ANGELES, 1972; NEW YORK; AM. INST. AERONAUT. ASTRONAUT.; DA. S.D.; VOL. 792; PP. 1-8; BIBL. 9 REF.Conference Paper

AKUSTISCHE UNTERSUCHUNGEN AN EINER EISENBAHNLINIE UND STUDIEN AM MODELL = ETUDE ACOUSTIQUE LE LONG D'UNE VOIE FERREE ET SUR UN MODELEWILMSEN G.1973; KAMPF DEM LAERM; DTSCH.; DA. 1973; VOL. 20; NO 2; PP. 46-47Serial Issue

MAXIMUM NOISE ABATEMENT TRAJECTORIES = TRAJECTOIRES D'AFFAIBLISSEMENT MAXIMUM DU BRUITZELDIN S; SPEYER J.1972; IN: AIAA 5TH FLUID PLASMA DYN. CONF. BOSTON, MASS., 1972; NEW YORK; AM. INST. AERONAUT. ASTRONAUT.; DA. 1972; VOL. 665; PP. 1-15; BIBL. 10 REF.Conference Paper

FLYOVER NOISE TESTING OF COMMERCIAL JET AIRPLANESZWIEBACK EL.sdIN: AIAA 4TH AIRCR. DES. FLIGHT TEST OPER. MEET. LOS ANGELES, 1972; NEW YORK; AM. INST. AERONAUT. ASTRONAUT.; DA. S.D.; VOL. 786; PP. 1-9; BIBL. 10 REF.Conference Paper

LA 28EME ASSEMBLEE GENERALE ANNUELLE DE L'IATA1972; INTERAVIA; SUISSE; DA. 1972; VOL. 27; NO 11; PP. 1192-1193Serial Issue

THE CF6 ENGINE. DESIGNED TO IMPROVE OPERATIONAL EFFECTIVENESSHEVENER RW.1971; S.A.E. TRANS.; U.S.A.; DA. 1971; VOL. 80; NO PART 4; PP. 2598-2611Serial Issue

AN ANALYSIS OF JET NOISE DIRECTIVITYPAO SP.sdIN: AIAA 11TH AEROSP. SCI. MEET.; WASHINGTON; 1973; NEW YORK; AM. INST. AERONAUT. ASTRONAUT.; DA. S.D.; VOL. 185; PP. 1-9; BIBL. 18 REF.Conference Paper

EASCON'72 RECORD. ELECTRONICS AND AEROSPACE SYSTEMS CONVENTION; WASHINGTON, D.C.; 19721972; NEW YORK, N.Y.; INST. ELECTR. ELECTRON. ENG.; DA. 1972; PP. 1-189Conference Paper

METHODES DE MESURE ET D'ANALYSE DU BRUIT DES AVIONS EN VOLAUZOLLE F; HAX J.1972; AERONAUT. ET ASTRONAUT.; FR.; DA. 1972; NO 33; PP. 17-28Serial Issue

ECONOMIC IMPACT OF APPLYING ADVANCED TECHNOLOGIES TO TRANSPORT AIRPLANES = IMPACT ECONOMIQUE DE L'APPLICATION DE TECHNOLOGIES AVANCEES AUX AVIONS DE TRANSPORTCARLINE AJK.sdIN: AIAA 4TH AIRCR. DES. FLIGHT TEST OPER. MEET. LOS ANGELES, 1972; NEW YORK; AM. INST. AERONAUT. ASTRONAUT.; DA. S.D.; VOL. 758; PP. 1-11; BIBL. 2 REF.Conference Paper

THERMODYNAMIC CONSIDERATIONS FOR THE DESIGN OF A SONIC-BOOM REDUCING POWERPLANTGALANIS N.1972; IN: AM. SOC. MECH. ENG. WINTER ANNU. MEET.; NEW YORK, N.Y.; 1972; S.L.; A.S.M.E.; DA. 1972; VOL. AERO-3; PP. 1-8; BIBL. 6 REF.Conference Paper

BRUIT RAYONNE PAR L'HELICE CARENEE DE L'AEROTRAIN 1-80SAURIER GH; DOYOTTE C.1972; REV. ACOUST.; FR.; DA. 1972; VOL. 5; NO SPEC; PP. 207-212; BIBL. 6 REF.Serial Issue

CALCULS DE PREVISION D'ATTENUATION DE CONDUITS ABSORBANTS ADAPTABLES A DES REACTEURS DOUBLE FLUXHAFFNER F.1972; REV. ACOUST.; FR.; DA. 1972; VOL. 5; NO SPEC; PP. 213-218Serial Issue

THE TRUCK NOISE PROBLEM AND WHAT MIGHT BE DONE ABOUT IT = LE PROBLEME DU BRUIT DES CAMIONS ET CE QUI POURRAIT ETRE FAIT A SON SUJETRINGHAM RF.1973; AUTOMOT. ENGNG; U.S.A.; DA. 1973; VOL. 81; NO 4; PP. 29-71 (4 P.)Serial Issue

COMMUNITIES ACT TO REDUCE THE IMPACT OF JET AIRCRAFT NOISEGOEDIKE W.1971; S.A.E. TRANS.; U.S.A.; DA. 1971; VOL. 80; PART 2; PP. 1442-1448; BIBL. 4 REF.Serial Issue

LEGAL ASPECTS OF AIRCRAFT NOISE AND SONIC BOOM IN THE UNITED STATESCHRISTOPHER W.1971; S.A.E. TRANS.; U.S.A.; DA. 1971; VOL. 80; PART 2; PP. 1421-1426; BIBL. 3 REF.Serial Issue

MEASUREMENT AND ANALYSIS OF ROTOR/PROPELLER NOISEIVES TR; LEVERTON JW.sdIN: CONF. REC. INTERPRETATION ENG. MEAS. PROC.; LONDON; 1972; LONDON; INST. MAR. ENG.; DA. S.D.; PP. 233-248 (9 P.); BIBL. 5 REF.Conference Proceedings

NOISE GENERATED BY STOL CORE-JET THRUST REVERSERSSTONE JR; GUTIERREZ OA.sdIN: AIAA 4TH AIRCR. DES. FLIGHT OPER. MEET. LOS ANGELES, 1972; NEW YORK; AM. INST. AERONAUT. ASTRONAUT.; DA. S.D.; VOL. 791; PP. 1-9; BIBL. 18 REF.Conference Paper

LOWERING DIESEL NOISE THROUGH HARDWARE MODIFICATIONSJENKINS SH; KUEHNER HK.1973; AUTOMOT. ENGNG; U.S.A.; DA. 1973; VOL. 81; NO 6; PP. 41-47Serial Issue

EFFECTS OF ROTATING FLOWS ON COMBUSTION AND JET NOISE = EFFETS D'ECOULEMENTS ROTATIFS SUR LA COMBUSTION ET SUR LE BRUIT D'UN JETSCHWARTZ IR.1972; IN: AIAA 5TH FLUID PLASMA DYN. CONF. BOSTON, MASS., 1972; NEW YORK; AM. INST. AERONAUT. ASTRONAUT; DA. 1972; VOL. 645; PP. 1-9; BIBL. 23 REF.Conference Paper

STUDIES INTO CONCORDE'S ENGINE NOISE EMISSION AND REDUCTIONHAWKINS R; HOCH R.1972; SEARCH; AUSTRAL.; DA. 1972; VOL. 3; NO 11-12; PP. 435-442Serial Issue

AN ACCEPTABLE EXPOSURE LEVEL FOR AIRCRAFT NOISE IN RESIDENTIAL COMMUNITIES = UN NIVEAU D'EXPOSITION ACCEPTABLE POUR LE BRUIT D'AVION DANS LES COMMUNAUTES RESIDENTIELLESYEOWART NS.1972; J. SOUND VIBRAT.; G.B.; DA. 1972; VOL. 25; NO 2; PP. 245-254; BIBL. 30REF.Serial Issue

ANALYTICAL AND EXPERIMENTAL SUPERSONIC JET NOISE RESEARCHKNOTT PR; BENZAKEIN MJ.sdIN: AIAA 11TH AEROSP. SCI. MEET.; WASHINGTON; 1973); NEW YORK; AM. INST. AERONAUT. ASTRONAUT.; DA. S.D.; VOL. 188; PP. 1-9; BIBL. 29 REF.Conference Paper