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BEITRAEGE ZUR STROEMUNGSMECHANIK UND FLUGMECHANIK. = CONTRIBUTIONS A LA MECANIQUE DES FLUIDES ET A LA MECANIQUE DU VOLWEISE A.1974; DTSCHE LUFT-U. RAUMFAHRT, FORSCH.-BER.; DTSCH.; DA. 1974; VOL. 74; NO 62; PP. (295P.); ABS. ANGL.; BIBL. DISSEM.Article

TECHNICAL EVALUATION REPORT ON AGARD FLIGHT MECHANICS PANEL SYMPOSIUM ON FLIGHT IN TURBULENCE.AIKEN WJ JR; LEAN D.1973; AGARD-AR-67; FR.; DA. 1973; PP. (9P.); (42ND FLIGHT MECH. PANEL MEET.; WOBURN ABBEY, BEDS.; 1973)Conference Proceedings

ISSLEDOVANIYA PO DINAMIKE POLETA KOSMICHESKIKH APPARATOV = ETUDE DE LA DYNAMIQUE DES VOLS DES SPATIONEFS1973; MOSKVA; NAUKA; DA. 1973; PP. 1-141; BIBL. DISSEM.Book

PERTURBATION METHODS IN ATMOSPHERIC FLIGHT MECHANICS = METHODES DE PERTURBATIONS EN MECANIQUE DU VOL ATMOSPHERIQUEZIPFEL PH.sdIN: AIAA 2ND ATMOS. FLIGHT MECH. CONF. PALO ALTO, CALIF., 1972; S.L.; AM. INST. AERONAUT. ASTRONAUT.; DA. S.D.; PP. 1-10; BIBL. 5 REF.Conference Paper

COMMENTAIRES SUR LES NORMES INTERNATIONALES ISO RELATIVES AUX "TERMES ET SYMBOLES DE LA MECANIQUE DE VOL"REBUFFET P.1973; AERONAUT. ET ASTRONAUT.; FR.; DA. 1973; NO 39; PP. 55-59; ABS. ANGL. ALLEMSerial Issue

PAPERS/AIAA ATMOSPHERIC FLIGHT MECHANICS CONFERENCE - AIAA AT 50, ANNIVERSARY CELEBRATION, ALBUQUERQUE NM, AUGUST 19-21, 19811981; ATMOSPHERIC FLIGHT MECHANICS CONFERENCE/1981-08-19/ALBUQUERQUE NM; USA; NEW YORK: AIAA; DA. 1981; 2 VOL.; 28 CMConference Proceedings

STABILITY CRITERIA FOR ACCELERATING AND DECELERATING AIRCRAFT = CRITERES DE STABILITE POUR UN AVION EN ACCELERATION OU EN DECELERATIONLAITONE EV; WEN FAN LIN.1973; J. AIRCR.; U.S.A.; DA. 1973; VOL. 10; NO 3; PP. 129-130; BIBL. 9 REF.Serial Issue

ANALYSIS OF R/V BEHAVIOR DURING BOUNDARY LAYER TRANSITION.CHRUSCIEL GT.1974; IN: AM. INST. AERONAUT. ASTRONAUT. 12TH AEROSP. SCI. MEET.; WASHINGTON; 1974; NEW YORK; A.I.A.A.; DA. 1974; VOL. 109; PP. 1-25; BIBL. 23 REF.Conference Paper

THE ROLE OF AERODYNAMICS AND DYNAMICS IN MILITARY AND CIVILIAN APPLICATIONS OF ROTARY WING AIRCRAFT = LE ROLE DE L'AERODYNAMIQUE ET DE LA DYNAMIQUE DANS LES APPLICATIONS MILITAIRES ET CIVILES DES AVIONS A VOILURE TOURNANTEYAGGY PF.1973; AGARD-LS-63; FR.; DA. 1973; PP. 1.1-1.14; (HELICOPTER AERODYN. DYN.; BRUSSELS; 1973)Conference Proceedings

AIAA 2ND ATMOSPHERIC FLIGHT MECHANICS CONFERENCE. PALO ALTO, CALIFORNIA, SEPTEMBER 11-13, 1972 = 2EME CONFERENCE AIAA SUR LA MECANIQUE DU VOL ATMOSPHERIQUE. PALO ALTO, CALIFORNIE, 11-13 SEPTEMBRE 1972sd; S.L.; AM. INST. AERONAUT. ASTRONAUT.; DA. S.D.; PP. (188 P.); BIBL. DISSEM.Conference Paper

TRUDELBEEINFLUSSUNG DURCH DIE "SUPERSTALL"-CHARAKTERISTIK = INFLUENCE DE LA CARACTERISTIQUE "SUPER DECROCHAGE" SUR LE PHENOMENE DE VRILLENEPPERT H.1972; Z. FLUGWISSENSCH.; DTSCH.; DA. 1972; VOL. 20; NO 11; PP. 414-421; ABS. ANGL. FR.; BIBL. 11 REF.Serial Issue

Computer model to study the effect of faulty controls on aircraft responseAL-BAHI, A. M; GHAZI, M. A.International journal of modelling & simulation. 1993, Vol 13, Num 3, pp 105-109, issn 0228-6203Article

Commande modale d'un avion sans pilote par retour dynamique de sortie = Numerical autopilot design by eigen structure assignmentBsalis, Elias; Bucharles, Alain.1992, 328 p.Thesis

Historical paper: Reflections on the Hohmann transferMIELE, A; CIARCIA, M; MATHWIG, J et al.Journal of optimization theory and applications. 2004, Vol 123, Num 2, pp 233-253, issn 0022-3239, 21 p.Article

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