TY  - BOOK
A1  - Bergmann, Ludwig
A1  - Schäfer, Clemens
A1  - Blome, Hans-Joachim
A1  - Gobrecht, Heinrich
ED  - Raith, Wilhelm
T1  - Lehrbuch der Experimentalphysik ; Bd. 8 : Sterne und Weltraum
Y1  - 1997
SN  - 3110151731
PB  - de Gruyter
CY  - Berlin [u.a.]
ER  - 
TY  - CHAP
A1  - Brandt, D.
A1  - Güsken, J.
A1  - Büchen, W.
A1  - [u.a.], 
A1  - Wahle, Michael
T1  - Konstruieren mit Aluminium [Kapitel 4]
T2  - Aluminium-Taschenbuch / Hrsg.: Aluminium-Zentrale Düsseldorf. - Bd. 3: Weiterverarbeitung und Anwendung
Y1  - 1997
SN  - 3-87017-243-6
SP  - 359
EP  - 544
PB  - Aluminium-Verlag
CY  - Düsseldorf
ET  - 15. Auflage
ER  - 
TY  - CHAP
A1  - Mertens, Josef
ED  - Sobieczky, H.
T1  - Certification of supersonic civil transports
T2  - New design concepts for high speed air transport. - (Courses and lectures / International Centre for Mechanical Sciences ; 366)
N2  - Since certification of Concorde new certification standards were introduced including many new regulations to improve flight safety. Most of these standards are to prevent severe accidents in the future which happened in the past (here: after Concorde’s certification). A new SCT has to fulfill these standards, although Concorde had none of these accidents. But accidents - although they sometimes occurred only for a specific aircraft type - have to be avoided for any (new) aircraft. Because of existing aircraft without typical accident types having demonstrated their reliability, they are allowed to go on based on their old certification; although sometimes new rules prevent accident types which are not connected to specific aircraft types - like e.g. evacuation rules. Anyway, Concorde is allowed to fly based on its old certification, and hopefully in the future will fly as safely as in the past. But a new SCT has to fulfill updated rules like any other aircraft, and it has to be “just another aircraft” [75].
KW  - Noise Exposure
KW  - Evacuation Rule
KW  - Severe Accident
KW  - Certification Rule
KW  - Thermal Fatigue Testing
Y1  - 1997
SN  - 3-2118-2815-X
U6  - http://dx.doi.org/10.1007/978-3-7091-2658-5_6
SP  - 97
EP  - 103
PB  - Springer
CY  - Wien [u.a.]
ER  - 
TY  - JOUR
A1  - Gerhardt, Hans Joachim
A1  - Krüger, O.
T1  - Building shape influence on local wind loads
JF  - Proceedings of the 2nd European & African Conference on Wind Engineering : 2 EACWE, Palazzo Ducale, Genova, Italy, June 22-26, 1997 / ed. by Giovanni Solari. - Vol. 2
Y1  - 1997
SN  - 88-86281-19-6
N1  - European and African Conference on Wind Engineering <2, 1997, Genova> ; ISBN für beide Bände
PB  - Servizi Grafici Editoriali
CY  - Padova
ER  - 
TY  - PAT
A1  - Schmitz, Günter
A1  - Schebitz, Michael
A1  - Esch, Thomas
T1  - Aus der Ruhelage selbstanziehender elektromagnetischer Aktuator
N2  - Elektromagnetischer Aktuator zur Betätigung eines Stellgliedes (2), mit wenigstens einem Elektromagneten (4) und einem mit dem Stellglied (2) verbundenen Anker (3), der gegen die Kraft einer Rückstellfeder (6) aus seiner Ruhelage in Richtung auf den Elektromagneten (4) bewegbar ist, mit einer Rückstellfeder (6), die eine nicht lineare, bezogen auf die Ruhelage des Ankers (3) progressiv ansteigende Kennlinie aufweist.
Y1  - 1997
N1  - Patent DE000019529152B4 2005.12.29
ER  - 
TY  - CHAP
A1  - Mertens, Josef
ED  - Sobieczky, H.
T1  - Aerodynamic multi point design challenge
T2  - New design concepts for high speed air transport.- (Courses and lectures / International Centre for Mechanical Sciences ; 366)
N2  - In the chapter “Son of Concorde, a Technology Challenge” one of the new challenges for a Supersonic Commercial Transport (SCT) is multi-point design for the four main design points:

- supersonic cruise
- transonic cruise
- take-off and landing
- transonic acceleration.
KW  - Drag Reduction
KW  - Pitching Moment
KW  - Leading Edge Vortex
KW  - Wave Drag
KW  - Variable Geometry
Y1  - 1997
SN  - 3-2118-2815-X
U6  - http://dx.doi.org/10.1007/978-3-7091-2658-5_4
SP  - 53
EP  - 67
PB  - Springer
CY  - Wien [u.a.]
ER  -