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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

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

SLOWLY OSCILLATING LIFTING SURFACES AT SUBSONIC AND SUPERSONIC SPEEDSBRUNE GW; DUSTO AR.1972; J. AIRCR.; U.S.A.; DA. 1972; VOL. 9; NO 11; PP. 777-783; BIBL. 21 REF.Serial Issue

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

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

EFFECTS OF JET DECAY RATE ON JET-INDUCED LOADS ON A FLAT PLATE.KUHLMAN JM; WARCUP RW.1978; J. AIRCR.; U.S.A.; DA. 1978; VOL. 15; NO 5; PP. 293-297; BIBL. 18 REF.Article

REYNOLDS NUMBER EFFECTS ON BOATTAIL DRAG OF WING-BODIES.REUBUSH DE.1977; J. AIRCR.; U.S.A.; DA. 1977; VOL. 14; NO 5; PP. 455-459; BIBL. 18 REF.Article

AN ALTERNATIVE TREATMENT OF BOUNDARY CONDITIONS FOR THE FLOW OVER THICK WINGS.NIXON D.1977; AERONAUT. QUART.; G.B.; DA. 1977; VOL. 28; NO 2; PP. 90-96; BIBL. 15 REF.Article

A CALCULATION METHOD FOR UNSTEADY SUBSONIC FLOW ABOUT HARMONICALLY OSCILLATING WING-BODY CONFIGURATIONS.ROOS R; BENNEKERS B; ZWAAN RJ et al.1975; IN: ANN. INST. AERONAUT. ASTRONAUT. 8TH FLUID PLASMA DYN. CONF.; HARTFORD, CONN.; 1975; NEW YORK; A.I.A.A.; DA. 1975; VOL. 864; PP. 1-10; BIBL. 12 REF.Conference Paper

TRANSONIC FLOW ABOUT LIFTING WING-BODY COMBINATIONS.BARNWELL RW.1974; IN: AM. INST. AERONAUT. ASTRONAUT. 12TH AEROSP. SCI. MEET.; WASHINGTON; 1974; NEW YORK; A.I.A.A.; DA. 1974; VOL. 185; PP. 1-13; H.T. 2; BIBL. 16 REF.Conference Paper

INSTATIONAERE DRUCKVERTEILUNGEN AN SCHWINGENDEN SCHLANKEN FLUEGEL-RUMPF-KOMBINATIONEN. VERGLEICH ZWISCHEN THEORIE UND MESSUNG. = DISTRIBUTIONS DES PRESSIONS INSTATIONNAIRES SUR LES CONFIGURATIONS AILE-FUSELAGE ELANCEES EN OSCILLATION. COMPARAISON DE LA THEORIE ET DES MESURESTRIEBSTEIN H; WAGENER J.1974; DTSCHE LUFT-U. RAUMFAHRT, FORSCH.-BER.; DTSCH.; DA. 1974; VOL. 74; NO 47; PP. 1-75; ABS. ANGL.; BIBL. 1 P. 1/2Article

COMPUTATIONAL TRANSONIC ANALYSIS FOR A SUPERCRITICAL TRANSPORT WING-BODY CONFIGURATIONWAGGONER EG.1980; AEROSPACE SCIENCES MEETING. 18/1980/PASADENA CA; USA; NEW YORK: AIAA; DA. 1980; 12 P.; BIBL. 11 REF.Conference Paper

CALCULS D'ECOULEMENTS TRANSSONIQUES AUTOUR D'UNE CONFIGURATION AILE-FUSELAGE DANS UNE APPROCHE PAR DOMAINESLE TH.1983; RECHERCHE AEROSPATIALE; ISSN 0034-1223; FRA; DA. 1983; NO 3; PP. 175-186; ABS. ENG; BIBL. 28 REF.Article

A LARGE-SCALE LOW-SPEED TUNNEL TEST OF A CANARD CONFIGURATION WITH SPANWISE BLOWING.JENKINS MWM; MEYER RT.1975; IN: AM. INST. AERONAUT. ASTRONAUT AIRCR. SYST. TECHNOL. MEET.; LOS ANGELES; 1975; NEW YORK; A.I.A.A.; DA. 1975; VOL. 994; PP. 1-9; BIBL. 2 REF.Conference Paper

STATE-OF-THE ART IN UNSTEADY AERODYNAMICS.RODDEN WP.1976; AGARD-R-650; FR.; DA. 1976; PP. (13P.); BIBL. 3 P. 1/2; (STRUCT. MATER. PANEL MEET. 43; LONDON; 1976)Report

CALCULATION OF NONLINEAR LIFT AND PITCHING MOMENT COEFFICIENTS FOR SLENDER WING-BODY COMBINATIONS.OTTO H.1974; J. AIRCR.; U.S.A.; DA. 1974; VOL. 11; NO 8; PP. 489-491; BIBL. 4 REF.Article

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

NONITERATIVE GRID GENERATION USING PARABOLIC DIFFERENCE EQUATIONS FOR FUSELAGEWING FLOW CALCULATIONSNAKAMURA S.1982; LECT. NOTES PHYS.; ISSN 0075-8450; DEU; DA. 1982; VOL. 170; PP. 396-401; BIBL. 3 REF.Conference Paper

CALCULATION OF UNSTEADY SUBSONIC FLOW ABOUT HARMONICALLY OSCILLATING WING/BODY CONFIGURATIONS.ROOS R; BENNEKERS B; ZWAAN RJ et al.1977; J. AIRCR.; U.S.A.; DA. 1977; VOL. 14; NO 5; PP. 447-454; BIBL. 13 REF.Article

THE MANY FACETS OF 3D TRANSONIC SHOCK-INDUCED SEPARATION. = LES MULTIPLES ASPECTS DU DECOLLEMENT INDUIT PAR UNE ONDE DE CHOC TRANSSONIQUE TRIDIMENSIONNELLEYOSHIHARA H; ZONARS D.1975; A.G.A.R.D. CONF. PROC.; FR.; DA. 1975; NO 168; PP. 42.1-42.8; BIBL. 3 REF.; (FLOW SEP. FLUID DYN. PANEL SYMP.; GOTTINGEN, GER.; 1975)Conference Paper

COMPUTATION OF PRESSURE DISTRIBUTION OF THE DFLVR WING-BODY MODEL BY THE PANEL METHODROMESH KUMAR JAIN; REDEKER G; SYED RAFEEQ AHMED et al.1980; D.F.V.L.R. FORSCH.-BER.; DEU; DA. 1980; VOL. 80; NO 2; 35 P.; ABS. GER; BIBL. 8 REF.Serial Issue

A FINITE ELEMENT SOLUTION OF UNSTEADY TRANSONIC FLOW PROBLEMS FOR THREE-DIMENSIONAL WINGS AND BODIES.KIMBLE KR.1976; IN: FLUID PLASMA DYN. CONF. 9; SAN DIEGO, CALIF.; 1976; NEW YORK; AM. INST. AERONAUT. ASTRONAUT.; DA. 1976; VOL. 328; PP. 1-11; BIBL. 10 REF.Conference Paper

AN IMPROVED METHOD FOR THE PREDICTION OF COMPLETELY THREE-DIMENSIONAL AERODYNAMIC LOAD DISTRIBUTIONS OF CONFIGURATIONS WITH LEADING EDGE VORTEX SEPARATION.JOHNSON FT; LU P; BRUNE GW et al.1976; IN: FLUID PLASMA DUN. CONF. 9; SAN DIEGO, CALIF.; 1976; NEW YORK; AM. INST. AERONAUT. ASTRONAUT.; DA. 1976; VOL. 417; PP. 1-7; BIBL. 19 REF.Conference Paper

EIN BEITRAG ZU DEN NICHTLINEAREN AUFTRIEBS- UND NICKMOMENTENEIGENSCHAFTEN VON SCHLANKEN FLUEGEL-RUMPF-KOMBINATIONEN. = CONTRIBUTION DE L'ETUDE DES CARACTERISTIQUES DE PORTANCE ET DE MOMENT DE TANGAGE NON LINEAIRES DES CONFIGURATIONS AILE MINCE-FUSELAGEHORST O.1974; Z. FLUGWISSENSCH.; DTSCH.; DA. 1974; VOL. 22; NO 6; PP. 188-200; ABS. ANGL. FR.; BIBL. 11 REF.Article

A FINITE ELEMENT METHOD FOR POTENTIAL AERODYNAMICS AROUND COMPLEX CONFIGURATIONS.LEE TZONG CHEN; SUCIU EO; MORINO L et al.1974; IN: AM. INST. AERONAUT. ASTRONAUT. 12TH AEROSP. SCI. MEET.; WASHINGTON; 1974; NEW YORK; A.I.A.A.; DA. 1974; VOL. 107; PP. 1-13; BIBL. 2 P. 1/2Conference Paper

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