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A FAST ALGORITHM FOR THE CALCULATION OF TRANSONIC FLOW OVER WING/BODY COMBINATIONSBAKER TJ; FORSEY CR.1983; AIAA J.; ISSN 0001-1452; USA; DA. 1983; VOL. 21; NO 1; PP. 60-67; BIBL. 18 REF.Article

CALCUL DES PRESSIONS A LA SURFACE D'UN FUSELAGE ET D'UNE AILE DANS UN FLUIDE IDEALMASLOV LA; YUSHIN VP.1977; IZVEST. AKAD. NAUK S.S.S.R., MEKH. ZHIDKOSTI GAZA; S.S.S.R.; DA. 1977; NO 3; PP. 110-115; BIBL. 4 REF.Article

AIRFRAME DESIGN TO REDUCE COMMUNITY NOISE.CORNING G; HALL JF.sdIN: ISR. ANNU. CONF. AVIAT. ASTRONAUT. 19; TEL AVIV, HAIFA, ISR.; 1977; JERUSALEM, ISR.; JERUSALEM ACAD. PRESS; DA. S.D.; PP. 14-24Conference Paper

PROBLEME DE L'ECOULEMENT SUPERSONIQUE SUR UN CORPS DE CONFIGURATION PRISMATIQUEVOROB'EV NF.1979; CHISLENN. METODY MEKH. SPLOSHN. SREDY; SUN; DA. 1979; VOL. 10; NO 3; PP. 25-27; BIBL. 5 REF.Article

FLOW SEPARATION OVER AXISYMMETRIC AFTERBODY MODELS.PRESZ WM JR; PITKIN ET.1974; J. AIRCR.; U.S.A.; DA. 1974; VOL. 11; NO 11; PP. 677-682; BIBL. 15 REF.Article

EXPERIMENTAL MEASUREMENT OF FIELDS EXCITED INSIDE THE FUSELAGE OF AN AIRCRAFTPERINI J.1980; I.E.E.E.E. TRANS. ELECTROMAGN. COMPATIB.; USA; DA. 1980; VOL. 22; NO 1; PP. 72-75; BIBL. 5 REF.Article

NUMERICAL SIMULATION OF WING-FUSELAGE INTERFERENCESHANG JS.1982; AIAA J.; ISSN 0001-1452; USA; DA. 1982; VOL. 20; NO 12; PP. 1657-1658; BIBL. 9 REF.Article

DESIGN STUDY OF STRUCTURAL CONCEPTS FOR AN ARROW-WING SUPERSONIC-CRUISE AIRCRAFT.SAKATA IF; DAVIS GW; ROBINSON JC et al.1975; IN: AM. INST. AERONAUT. ASTRONAUT. AIRCR. SYST. TECHNOL. MEET.; LOS ANGELES; 1975; NEW YORK; A.I.A.A.; DA. 1975; VOL. 1037; PP. 1-12; BIBL. 3 REF.Conference Paper

COMPOSITE CENTER FUSELAGE PHASE IMURRIN LJ; ERBACHER H.1980; RISING TO THE CHALLENGE. SPI ANNUAL CONFERENCE. 35/1980/NEW ORLEANS LA; USA; NEW YORK: SPI; DA. 1980; PP. 12.B.1-12.B.5; BIBL. 11 REF.Conference Paper

CHARACTERISTICS OF PROPELLER NOISE ON AN AIRCRAFT FUSELAGEKEARNEY BARTON C; MIXSON JS.1981; J. AIRCR.; ISSN 0021-8669; USA; DA. 1981; VOL. 18; NO 3; PP. 200-205; BIBL. 13 REF.Article

ARE WHEEL-WELL RELATED AEROACOUSTIC SOURCES OF ANY SIGNIFICANCE IN AIRFRAME NOISE.DOBRZYNSKI WM; HELLER HH.1978; Z. FLUGWISSENSCH. WELTR.-FORSCH.; DTSCH.; DA. 1978; VOL. 2; NO 1; PP. 35-42; ABS. ALLEM.; BIBL. 7 REF.Article

LOW-FREQUENCY PRESSURE FLUCTUATIONS IN AXISYMMETRIC TURBULENT BOUNDARY LAYERSPANTON RL; GOLDMAN AL; LOWERY RL et al.1980; J. FLUID MECH.; GBR; DA. 1980; VOL. 97; NO 2; PP. 299-319; BIBL. 23 REF.; 1 ILL.Article

IDENTIFICATION OF VOLTAGE TRANSIENTS ON AIRCRAFT CABLING UNDER LTA EXCITATIONMCCORMICK WS; MAXWELL KJ.1979; I.E.E.E. TRANS. AEROSPACE ELECTRON. SYST.; USA; DA. 1979; VOL. 15; NO 3; PP. 372-377; BIBL. 2 REF.Article

Research challenges arising from current and potential applications of dynamic fracture mechanics to the integrity of engineering structuresKANNINEN, M. F; O'DONOGHUE, P. E.International journal of solids and structures. 1995, Vol 32, Num 17-18, pp 2423-2445, issn 0020-7683Conference Paper

A SEMIEMPIRICAL METHOD FOR PREDICTING NORMAL FORCE AND CENTRE OF PRESSURE CHARACTERISTICS OF WING BODY COMBINATIONS AT SUPERSONIC SPEEDS INCLUDING THE NONLINEAR EFFECTS OF BODY CROSSFLOW.SHANKA NARAYAN SESHADRI.1977; DTSCHE LUFT- U. RAUMFAHRT, FORSCH.-BER.; DTSCH.; DA. 1977; VOL. 77; NO 7; PP. 1-44; ABS. ALLEM.; BIBL. 1 P.Serial Issue

CALCULATION OF FORCES ON STORES IN THE VICINITY OF AIRCRAFT = CALCUL DES FORCES S'EXERCANT SUR DES CHARGES EXTERNES DANS LE VOISINAGE D'UN AVIONSERBIN H.1973; J. AIRCR.; U.S.A.; DA. 1973; VOL. 10; NO 2; PP. 123-124; BIBL. 4 REF.Serial Issue

EFFECT OF AIR FLOW, PANEL CURVATURE, AND INTERNAL PRESSURIZATION ON FIELD-INCIDENCE TRANSMISSION LOSS.KOVAL LR.1976; J. ACOUST. SOC. AMER.; U.S.A.; DA. 1976; VOL. 59; NO 6; PP. 1379-1385; BIBL. 24 REF.Article

Multi-level optimization of aircraft shell structuresROTHWELL, A.Thin-walled structures. 1990, Vol 11, Num 1-2, pp 85-103, issn 0263-8231, 19 p.Article

ETUDE DE L'EFFET D'INTERFERENCE D'UNE AILE TRIANGULAIRE ET D'UN DEMI-CORPSKOSYACHENKO K YA; SHCHERBAKOV GK.1976; VEST. LENINGRAD. UNIV.; S.S.S.R.; DA. 1976; NO 13; PP. 82-89; ABS. ANGL.; BIBL. 4 REF.Article

IMAGE SYSTEM SOLUTION FOR STORE AERODYNAMICS WITH INTERFERENCE. II.MARTIN FW; WALKLEY KB.1975; J. AIRCR.; U.S.A.; DA. 1975; VOL. 12; NO 3; PP. 156-161; BIBL. 4 REF.Article

STEADY AND OSCILLATORY SUBSONIC AND SUPERSONIC AERODYNAMICS AROUND COMPLEX CONFIGURATIONS.MORINO L; LEE TZONG CHEN; SUCIU EO et al.1975; A.I.A.A. J., NEW YORK; U.S.A.; DA. 1975; VOL. 13; NO 3; PP. 368-374; BIBL. 28 REF.Article

SICHTBARMACHUNG DER UMSTROEMUNG ZWEIER RAUMGLEITERKONFIGURATIONEN IM UNTERSCHALLBEREICH. = VISUALISATION DE L'ECOULEMENT AUTOUR DE DEUX PROFILS DANS LE DOMAINE SUBSONIQUEBIPPES H; COLAK ANTIC P.1975; DTSCHE LUFT- U. RAUMFAHRT, FORSCH.-BER.; DTSCH.; DA. 1975; VOL. 75; NO 49; PP. 1-45; H.T. 14; ABS. ANGL.; BIBL. 2 P.Serial Issue

THEORETICAL AND EXPERIMENTAL EVALUATION OF TRANSMISSION LOSS OF CYLINDERSWANG YS; CROCKER MJ; RAJU PK et al.1983; AIAA JOURNAL; ISSN 0001-1452; USA; DA. 1983; VOL. 21; NO 2; PP. 186-192; BIBL. 15 REF.Article

AIRFRAME NOISE MEASUREMENTS ON A SUPERSONIC TEANSPORT SMALL-SCALE MODELPREISSER JS.1980; J. AIRCR.; ISSN 0021-8669; USA; DA. 1980; VOL. 17; NO 11; PP. 795-801; BIBL. 15 REF.Article

THE ANALYSIS AND IDENTIFICATION OF FLUX-INDUCED VOLTAGE TRANSIENTS ON LOW-LOSS TRANSMISSION LINES WITH APPLICATION TO THE LIGHTNING-TRANSIENT-ANALYSIS (LTA) PROBLEMMCCORMICK WS.1979; I.E.E.E. TRANS. ELECTROMAGN. COMPATIB.; USA; DA. 1979; VOL. 21; NO 1; PP. 13-19; BIBL. 6 REF.Article

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