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TRAGENDE SCHNABELPROFILE IN STOSSFREIER SCHALLANSTROEMUNG. = PROFILS PORTANTS A BORDS D'ATTAQUE AIGUS DANS UN ECOULEMENT INCIDENT TRANSSONIQUE SANS CHOCSOBIECZKY H.1975; Z. ANGEW. MATH. PHYS.; SCHWEIZ; DA. 1975; VOL. 26; NO 6; PP. 819-830; ABS. ANGL.; BIBL. 4 REF.Article

ENTWURF UEBERKRISTISCHER PROFILE MIT HILFE DER RHEOELEKTRISCHEN ANALOGIE. = PROJET DE PROFILS SUPER-CRITIQUES A L'AIDE DE L'ANALOGIE RHEOELECTRIQUESOBIECZKY H.1975; DTSCHE LUFT-U. RAUMFAHRT, FORSCH.-BER.; DTSCH.; DA. 1975; VOL. 75; NO 43; PP. 1-51; ABS. ANGL.; BIBL. 2 P.Article

DESIGN OF ADVANCED TECHNOLOGY TRANSONIC AIRFOILS AND WINGSSOBIECZKY H.1980; AGARD CONF. PROC.; ISSN 0549-7191; FRA; DA. 1980; NO 285; 13 P.; BIBL. 32 REF.Conference Paper

DIE BERECHNUNG LOKALER RAEUMLICHER UEBERSCHALLFELDER = LE CALCUL DU CHAMP SUPERSONIQUE LOCAL DANS L'ESPACESOBIECZKY H.1978; Z. ANGEW. MATH. MECH.; DDR; DA. 1978; VOL. 58; NO 7; PP. 331-333; BIBL. 4 REF.Article

Analytical tools for systematic transonic designSOBIECZKY, H.International journal for numerical methods in engineering. 1986, Vol 22, Num 2, pp 309-326, issn 0029-5981Article

SHOCKLESS DESIGN AND ANALYSIS OF TRANSONIC CASCADE SHAPESDULIKRAVICH DS; SOBIECZKY H.1982; AIAA J.; ISSN 0001-1452; USA; DA. 1982; VOL. 20; NO 11; PP. 1572-1578; BIBL. 18 REF.Article

SHOCK OBLIQUITY EFFECT ON TRANSONIC SHOCK-BOUNDARY LAYER INTERACTIONINGER GR; SOBIECZKY H.1978; Z. ANGEW. MATH. MECH.; DDR; DA. 1978; VOL. 58; NO 7; PP. 333-335; BIBL. 5 REF.Article

INVISCID-VISCOUS INTERACTIONS IN THE NEARLY DIRECT DESIGN OF SHOCK-FREE SUPERCRITICAL AIRFOILSNEBECK HE; SEEBASS AR; SOBIECZKY H et al.1981; AGARD CONF. PROC.; ISSN 0549-7191; FRA; DA. 1981; NO 291; PP. 3.1-3.10; BIBL. 21 REF.Article

A NEW METHOD FOR DESIGNING SHOCK-FREE TRANSONIC CONFIGURATIONSSOBIECZKY H; YU NJ; FUNG KY et al.1978; AMERICAN INSTITUTE OF AERONAUTICS AND ASTRONAUTICS FLUID AND PLASMA DYNAMIC CONFERENCE. 11/1978/SEATTLE WA; USA; NEW YORK: AIAA; DA. 1978; 78-1114; 33 P.; BIBL. 21 REF.Conference Paper

NEW METHOD FOR DESIGNING SHOCK-FREE TRANSONIC CONFIGURATIONSSOBIECZKY H; YU NJ; FUNG KY et al.1979; A.I.A.A.J., NEW YORK; USA; DA. 1979; VOL. 17; NO 7; PP. 722-729; BIBL. 23 REF.Article

Subsonic airfoils with a given pressure distributionHASSAN, A; SOBIECZKY, H; SEEBASS, A. R et al.AIAA journal. 1984, Vol 22, Num 9, pp 1185-1191, issn 0001-1452Article

Manual aerodynamic optimization of an oblique wing supersonic transportPEI LI; SOBIECZKY, H; SEEBASS, R et al.Journal of aircraft. 1999, Vol 36, Num 6, pp 907-913, issn 0021-8669Conference Paper

The DFVLR-5 wing experiment: towards the validation of the numerical simulation of transonic viscous wing flowsKORDULLA, W; SCHWAMBORN, D; SOBIECZKY, H et al.AGARD conference proceedings. 1988, Vol 1, Num 437, pp 13.1-13.18, issn 0549-7191Conference Paper

Supercritical cascade flow analysis with shock-boundary layer interaction and shock-free redesignNIEDERDRENK, P; SOBIECZKY, H; DULIKRAVICH, G. S et al.Journal of turbomachinery. 1987, Vol 109, Num 3, pp 413-419, issn 0889-504XArticle

Shock-free transonic airfoils with a given pressure distributionHASSAN, A. A; SOBIECZKY, H; SEEBASS, A. R et al.Computer methods in applied mechanics and engineering. 1986, Vol 58, Num 3, pp 285-304, issn 0045-7825Article

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