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MECANISME DE FORMATION DE LA FORCE NORMALE POUR UN BATTEMENT D'AILESBELOTSERKOVSKIJ SM; GULYAEV VV; NISHT MI et al.1974; IN: IZBR. PROBL. PRIKL. MEKH.; MOSKVA; VINITI; DA. 1974; PP. 97-102; BIBL. 8 REF.Book Chapter

UNSTEADY AERODYNAMICS OF VEHICLES IN TUBES.HAMMITT AG.1975; A.I.A.A. J., NEW YORK; U.S.A.; DA. 1975; VOL. 13; NO 4; PP. 497-503; BIBL. 7 REF.Article

RECENT ADVANCES IN TECHNIQUES FOR DYNAMIC STABILITY AT NAE.ORLIK RUCKEMANN KJ.1976; QUART. BULL. DIV. MECH. ENGNG NATION. AERONAUT. ESTABL.; CANADA; DA. 1976; NO 1; PP. 1-22; BIBL. 15 REF.Article

UNSTEADY AERODYNAMICS.1978; A.G.A.R.D. CONF. PROC.; FRA; DA. 1978; NO 227; (312 P.); ABS. ENG; BIBL. DISSEM.Serial Issue

SOME NOTES ON UNSTEADY LIFTING-LINE THEORY.VAN HOLTEN T.1976; J. FLUID MECH.; G.B.; DA. 1976; VOL. 77; NO 3; PP. 561-579; BIBL. 9 REF.Article

EIN INSTATIONAERES VERHALTEN TRANSSONISCHER STROEMUNGEN. = UN COMPORTEMENT INSTATIONNAIRE DES ECOULEMENTS TRANSSONIQUESMEIER GEA.1974; MITT. MAX-PLANCK-INST. STROEMUNGSFORSCH. AERODYN. VERSUCHSANST.; DTSCH.; DA. 1974; NO 59; PP. (138P.); BIBL. 5 P.Article

STUDY OF THE UNSTEADY AERODYNAMICS OF LIFTING SURFACES USING THE COMPUTER.BELOTSERKOVSKII SM.1977; ANNU. REV. FLUID MECH.; U.S.A.; DA. 1977; VOL. 9; PP. 469-494; BIBL. 3 P.Article

METHODES D'ESSAIS DE GRILLES D'AUBES EN SOUFFLERIE A L'ONERALEYNAERT J.1977; BULL. ASS. TECH. MARIT. AERONAUT.; FRA; DA. 1977; NO 33; PP. 289-299; ABS. ENG; BIBL. 3 REF.Article

NUMERICAL EVALUATION OF THE THREE-DIMENSIONAL HARMONIC KERNEL.JORDAN PF.1976; Z. FLUGWISSENSCH.; DTSCH.; DA. 1976; VOL. 24; NO 4; PP. 205-209; ABS. ALLEM. FR.; BIBL. 6 REF.Article

CALCUL DES CARACTERISTIQUES AERODYNAMIQUES NON STATIONNAIRES DE SYSTEMES PORTEURS TRIDIMENSIONNELSPOPYTALOV SA.1976; IZVEST. AKAD. NAUK S.S.S.R., MEKH. ZHIDKOSTI GAZA; S.S.S.R.; DA. 1976; NO 1; PP. 173-176; BIBL. 8 REF.Article

PORTANCES INSTATIONNAIRES SUR UN CYLINDRE VIBRANT DANS UN ECOULEMENT SUPERCRITIQUE.SZECHENYI E; LOISEAU H.1975; RECH. AEROSPAT.; FR.; DA. 1975; NO 1; PP. 45-57; ABS. ANGL.; BIBL. 11 REF.Article

UNSTEADY SUPERSONIC AERODYNAMIC THEORY BY THE METHOD OF POTENTIAL GRADIENT.JONES WP; APPA K.1977; A.I.A.A.J., NEW YORK; U.S.A.; DA. 1977; VOL. 15; NO 1; PP. 59-65; BIBL. 23 REF.Article

SIMULATION DU FLOTTEMENT AU SOL POUR LES AVIONS DE GRAND ALLONGEMENT.RAJAGOPAL P.1974; AO-CNRS-11849; FR.; DA. 1974; PP. 1-90; ABS. ANGL.; BIBL. 2 P.; (THESE DOCT.-ING.; PARIS VI)Thesis

THEORIE NON LINEAIRE NON STATIONNAIRE DE L'AILE MINCE DE FORME EN PLAN ARBITRAIREBELOTSERKOVSKIJ SM; NISHT MI.1974; IZVEST. AKAD. NAUK S.S.S.R., MEKH. ZHIDKOSTI GAZA; S.S.S.R.; DA. 1974; NO 4; PP. 100-108; BIBL. 11 REF.Article

SMALL PERTURBATION EXPANSIONS IN UNSTEADY AEROFOIL THEORY.GRAHAM JMR; KULLAR I.1977; J. FLUID MECH.; G.B.; DA. 1977; VOL. 83; NO 2; PP. 209-224; BIBL. 22 REF.Article

UNSTEADY AERODYNAMIC MODELING FOR ARBITRARY MOTIONS.EDWARDS JW.1977; A.I.A.A. J., NEW YORK; U.S.A.; DA. 1977; VOL. 15; NO 4; PP. 593-595; BIBL. 6 REF.Article

UNSTEADY AIRLOADS IN SEPARATED AND TRANSONIC FLOW. AGARD STRUCTURES AND MATERIALS PANEL. MEETING. 44; LISBON; 1977.1977; A.G.A.R.D. CONF. PROC.; FR.; DA. 1977; NO 226; PP. (256P.); BIBL. DISSEM.Conference Paper

PARTICULAR PROBLEMS OF DATA ACQUISITION AND ANALYSIS.1976; A.G.A.R.D. CONF. PROC.; FR.; DA. 1976; NO 210; PP. (20P.); BIBL. DISSEM.; (NUMER. METHODS WINDTUNNEL TEST. FLUID DYN. PANEL SPEC. MEET.; RHODE-ST-GENESE, BELG.; 1976)Conference Paper

RECENT DEVELOPMENTS IN PREDICTING UNSTEADY AIRLOADS CAUSED BY CONTROL SURFACE MOTIONS.ROWE WS; SEBASTIAN JD; REDMAN MC et al.1976; J. AIRCR.; U.S.A.; DA. 1976; VOL. 13; NO 12; PP. 955-961; BIBL. 9 REF.Article

UNSTEADY WAKE MEASUREMENTS OF AIRFOILS AND CASCADES.SATYANARAYANA B.1977; A.I.A.A.J., NEW YORK; U.S.A.; DA. 1977; VOL. 15; NO 5; PP. 613-618; BIBL. 15 REF.Article

NUMERICAL COMPUTATION OF NONSTATIONARY AERODYNAMICS OF FLAT PLATE CASCADES IN COMPRESSIBLE FLOW.NI RH; SISTO F.1975; IN: GAS TURBINE CONF. PROD. SHOW; HOUSTON, TEX.; 1975; NEW YORK; AM. SOC. MECH. ENG.; DA. 1975; VOL. 75-GT5; PP. 1-6; BIBL. 17 REF.Conference Paper

UNSTEADY AERODYNAMICS OF SLENDER DELTA WINGS AT LARGE ANGLES OF ATTACK.ERICSSON LE; REDING JP.1975; J. AIRCR.; U.S.A.; DA. 1975; VOL. 12; NO 9; PP. 721-729; BIBL. 41 REF.Article

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

CALCUL DES CARACTERISTIQUES AERODYNAMIQUES D'UNE AILE SE DEPLACANT A UNE VITESSE SUBSONIQUE DANS LE CAS D'UNE FAIBLE ACTION DE L'ONDE DE CHOCGRITSENKO NA; NISHT MI.1977; IZVEST. AKAD. NAUK S.S.S.R., MEKH. ZHIDKOSTI GAZA; S.S.S.R.; DA. 1977; NO 4; PP. 149-154; BIBL. 4 REF.Article

FLUTTER AND GUST RESPONSE ANALYSIS OF FLEXIBLE AIRCRAFT WITH ACTIVE CONTROL.NOLL RB; MORINO L.1976; IN: STRUCT. STRUCT. DYN. MATER. CONF. 17. PROC.; KING OF PRUSSIA, PA.; 1976; S.L.; AM. INST. AERONAUT. ASTRONAUT.; DA. 1976; PP. 389-397; BIBL. 14 REF.Conference Paper

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