Review of multivariable control applied to the VAAC Harrier and remaining open questionsHYDE, Rick A.Lecture notes in control and information sciences. 2006, pp 183-202, issn 0170-8643, isbn 3-540-31754-6, 1Vol, 20 p.Conference Paper

CASA 212 AVIOCAR1973; INTERAVIA; SUISSE; DA. 1973; VOL. 28; NO 4; PP. 355Serial Issue

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PREDICTION METHODS FOR JET V/STOL PROPULSION AERODYNAMICS.PLATZER MF; MARGASON RJ.1978; J. AIRCR.; U.S.A.; DA. 1978; VOL. 15; NO 2; PP. 69-77; BIBL. 1 P. 1/2Article

LE HS.146. UN NOUVEAU CONCURRENT SUR ETAPES COURTES1973; INTERAVIA; SUISSE; DA. 1973; VOL. 28; NO 8; PP. 887-888Serial Issue

ATC SYSTEM PLANNING FOR V*STOL AVIATIONRICHARDSON RA.1973; I.E.E.E. TRANS. COMMUNIC.; U.S.A.; DA. 1973; VOL. 21; NO 5; PP. 529-531Serial Issue

DIE BEDEUTUNG DER AERODYNAMISCHEN STRAHL-INTERFERENZ BEI DER ENTWICKLUNG UND ERPROBUNG DES V/STOL-TRANSPORTFLUGZEUGES DO 31 = LA SIGNIFICATION DE L'INTERFERENCE DANS LA REACTION AERODYNAMIQUE, LE DEVELOPPEMENT ET LE CONTROLE DE L'APPAREIL DE TRANSPORT ADAC/V DO 31WELTE D.sdIN: 5. JAHRESTAG. DTSCH. GES. LUFT RAUMFAHRT; BERLIN; 1972; S.L.; DA. S.D.; PP. 1-14; H.T. 10; BIBL. 2 REF.Conference Paper

DREIKOMPONENTENMESSUNGEN AM MODELL EINES LEICHTEN STOL-FLUGZEUGS MIT AUSBLASEN IN FLUEGELTIEFENRICHTUNG. = MESURES A TROIS COMPOSANTES SUR UNE MAQUETTE D'AVION LEGER DE TYPE ADAC AVEC SOUFFLAGE A L'INTERIEUR DE L'AILEKORNER H; LOHR R.1975; DTSCHE LUFT- U. RAUMFAHRT, FORSCH.-BER.; DTSCH.; DA. 1975; VOL. 75; NO 74; PP. 1-21; ABS. ANGL.; BIBL. 8 REF.Serial Issue

ADVANCED TECHNOLOGY FOR STOL TRANSPORTSCORNISH JJ III.1971; S.A.E. TRANS.; U.S.A.; DA. 1971; VOL. 80; NO PART 4; PP. 2497-2506Serial Issue

BENEFIT-COST ANALYSIS OF DELAY REDUCTION WITH STOLBARRIAGE JB; PRICE SPE.1973; PROC. AMER. SOC. CIV. ENGRS, TRANSPORT. ENGNG J. A.S.C.E.; U.S.A.; DA. 1973; VOL. 99; NO 1; PP. 43-52; BIBL. 11 REF.Serial Issue

A BASIC STUDY OF THE STOL GROUND EFFECT PROBLEM FOR PLANAR FLOW.KOTANSKY DR; BOWER WW.1978; J. AIRCR.; U.S.A.; DA. 1978; VOL. 15; NO 4; PP. 214-221; BIBL. 6 REF.Article

ZUR ENTWICKLUNG SENKRECHT STARTENDER FLUGZEUGE = DEVELOPPEMENT DES AVIONS ADAVKUNZLER M.1973; SCHWEIZ. BAUZTG; SCHWEIZ; DA. 1973; VOL. 91; NO 8; PP. 181-182Serial Issue

PREDICTION OF GROUND EFFECTS FOR VTOL AIRCRAFT WITH TWIN LIFTING JETS.LOUISSE J; MARSHALL F.1976; J. AIRCR.; U.S.A.; DA. 1976; VOL. 13; NO 2; PP. 123-127; BIBL. 14 REF.Article

L'AUGMENTATION DE POUSSEE DES TROMPES A JETS PULSANTS OU BATTANTS.DIDELLE H.1976; GRENOBLE; DA. 1976; PP. 1-249; BIBL. 4 P. 1/2; (THESE DOCT.-ING.; UNIV. SCI. MED. GRENOBLE)Thesis

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CHOICES FOR THE FUTURE: AN INDUSTRY VIEWPOINT ON PROTOTYPING = CHOIX POUR LE FUTUR: POINT DE VUE DE L'INDUSTRIE SUR L'UTILISATION DES PROTOTYPESALTIS HD.1972; IN: SOC. AUTOMOT. ENG. NATL. AEROSP. ENG. MANUF. MEET.; SAN DIEGO, CALIF.; 1972; NEW YORK; SOC. AUTOMOT. ENG.; DA. 1972; VOL. 848; PP. 1-6Conference Paper

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

THE ATTACHMENT OF A VENTILATED PLANE JET TO AN INCLINED PLANE WALLMARSTERS GF.1978; AERONAUT. QUART.; GBR; DA. 1978; VOL. 29; NO 2; PP. 60-74; BIBL. 4 REF.Article

DESIGN STUDIES OF LOW-NOISE PROPULSIVE-LIFT AIRPLANESSWEET HS; LESLIE HR; BENNETT JA et al.1973; S.A.E. TRANS.; U.S.A.; DA. 1973; VOL. 82; NO 2; PP. 1321-1331; BIBL. 11 REF.Article

NASA LIFT FAN V/STOL TRANSPORT TECHNOLOGY STATUS = ETAT DE LA TECHNOLOGIE DU TRANSPORT ADAC/V A SOUFFLANTE DE SUSTENTATION A LA NASADECKERT WH; EVANS RC.1972; IN: SOC. AUTOMOT. ENG. NATL. AEROSP. ENG. MANUF. MEET.; SAN DIEGO, CALIF.; 1972; NEW YORK; SOC. AUTOMOT. ENG.; DA. 1972; VOL. 856; PP. 1-7; H.T. 5; BIBL. 6 REF.Conference Paper

CHARACTERISTICS OF AN EJECTOR-TYPE ENGINE SIMULATOR FOR STOL MODEL TESTING = CARACTERISTIQUES D'UN SIMULATEUR DE MOTEUR DU TYPE A EJECTION POUR L'ESSAI DE MODELES D'ADACNICOLOFF GB; WEBER HA.sdIN: AIAA 7TH AERODYN. TEST. CONF. PALO ALTO, CALIF., 1972; NEW YORK; AM. INST. AERONAUT. ASTRONAUT.; DA. S.D.; NO 993; PP. 1-8; BIBL. 3 REF.Conference Paper

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VSTOL Aircraft market analysisHOWARTH, D. K.Aeronautical Journal. 2009, Vol 113, Num 1140, pp 107-118, issn 0001-9240, 12 p.Conference Paper

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