TY  - JOUR
A1  - Wittmann, Klaus
A1  - Feuerbacher, B.
A1  - Ulamec, S.
A1  - Rosenbauer, H. (u.a.)
T1  - Rosetta Lander - In Situ Characterisation of a Comet Nucleus
JF  - Acta Astronautica. 45 (1999), H. 4-9
Y1  - 1999
SN  - 0094-5765
SP  - 389
EP  - 395
ER  - 
TY  - JOUR
A1  - Mertens, Josef
A1  - Kelm, R.
A1  - Velden, A. van der
T1  - Interdisziplinäre Auslegung eines Verkehrsflugzeugflügels
JF  - DGLR-Jahrbuch 1999 Bd. 3
Y1  - 1999
N1  - DGLR-JT99-156
SP  - 1605
EP  - 1610
ER  - 
TY  - JOUR
A1  - Mertens, Josef
T1  - Einige herausragende Ergebnisse des Technologieprogramms "Reduktion des Aerodynamischen Widerstands (RaWid)"
JF  - DGLR-Jahrbuch 1999 Bd. 3
Y1  - 1999
N1  - DGLR-JT99-047
SP  - 1461
EP  - 1468
ER  - 
TY  - BOOK
A1  - Mertens, Josef
T1  - Reduktion des aerodynamischen Widerstands (RaWid) : Abschlußbericht ; Laufzeit des Vorhaben, Berichtszeitraum: 01.07.1995 bis 31.12.1998 / Verf.: J. Mertens
Y1  - 1999
N1  - Förderkenzeichen BMBF 20 A 9595 A. Engl. Zsfassung u.d.T.: Reduction of aerodynamis drag (RaWid) - final report . auch als elektronisches Dokument vorh.
PB  - DaimlerChrysler Aerospare Airbus GmbH
CY  - Hamburg
ER  - 
TY  - BOOK
A1  - Mertens, Josef
T1  - Reduktion des aerodynamischen Widerstands (RaWid) : Abschlußbericht ; Laufzeit des Vorhaben, Berichtszeitraum: 01.07.1995 bis 31.12.1998 / Verf.: J. Mertens
Y1  - 1999
N1  - Parallel als gedruckte Ausgabe erschienen
PB  - DaimlerChrysler Aerospare Airbus GmbH
CY  - Hamburg
ER  - 
TY  - JOUR
A1  - Bohn, D.
A1  - Funke, Harald
A1  - Gier, J.
T1  - Temperature jet development in a cross-over channel
JF  - Third European Conference on Turbomachinery - fluid dynamics and thermodynamics : : 2 - 5 March 1999, Royal National Hotel, London, UK / organized by the Energy Transfer and Thermofluid Mechanics Group of the Institution of Mechanical Engineers (IMechE); with support and sponsorship from European Commission / Vol. B.
Y1  - 1999
N1  - C557/158/99 ; IMechE conference transactions 1999-1B
SP  - 671
EP  - 680
PB  - Professional Engineering Publ.
CY  - Bury St. Edmunds
ER  - 
TY  - JOUR
A1  - Bohn, D.
A1  - Funke, Harald
A1  - Gier, J.
T1  - Numerical and Experimental Investigations on the Flow in a 4-Stage Turbine with Special Focus on the Development of a Radial Temperature Streak
JF  - ASME Turbo Expo 1999, Indianapolis, USA, 1999
Y1  - 1999
N1  - ASME-Paper 99-GT-027
ER  - 
TY  - BOOK
A1  - Wahle, Michael
T1  - Angewandte Strukturanalyse. - (Dynamik)
Y1  - 1999
SN  - 3-89653-567-6
PB  - Mainz
CY  - Aachen
ER  - 
TY  - CHAP
A1  - Mertens, Josef
ED  - Nitsche, Wolfgang
T1  - Some important results of the technology programme RaWid
T2  - New Results in Numerical and Experimental Fluid Mechanics : Contributions to the 11th AG STAB/DGLR Symposium Berlin, Germany 1998. - Vol. 2. - (Notes on Numerical Fluid Mechanics ; 72)
Y1  - 1999
SN  - 978-3-663-10903-7 (Print)
SN  - 978-3-663-10901-3 (Elektronisch)
U6  - http://dx.doi.org/10.1007/978-3-663-10901-3_41
SP  - 315
EP  - 322
PB  - Springer Fachmedien
CY  - Wiesbaden
ER  - 
TY  - CHAP
A1  - Mertens, Josef
T1  - Laminar leading edges: manufacturing, contamination, and operational aspects - results from the German RaWid programme
N2  - RaWid was the German national technology programme on transonic aerodynamics and supporting technologies, lasting from 1995 to 1998. One of the main topics was laminar wing development. Besides aerodynamic design work, many operational aspects were investigated. A manufacturing concept was developed to be applied to operational laminar wings and empennages. It was built in a large scale manufacturing demonstrator with the aerodynamic shape of a 1,5 m section of the A320 fin nose. Tolerances in shape and roughness fulfilled all requirements. The construction can easily be adapted to varying stiffness and strength requirements. Weight and manufacturing costs are comparable to common nose designs. The mock-up to be designed in ALTTA is based on this manufacturing principle. Another critical point is contamination of suction surfaces. Several tests were performed to investigate perforated titanium suction surfaces at realistic operational conditions: - a one year flight test with a suction plate in the stagnation area of the Airbus "Beluga" - a one year test of several suction plates in a ground test near the airport - a one year test of a working suction ground test installation at all weather conditions. No critical results were found. There is no long term suction degradation visible. Icing conditions and ground de-icing fluids used on airports did not pose severe problems. Some problems detected require only respection of weak design constraints.
KW  - Laminare Strömung
KW  - Ansaugsystem
KW  - Profilumströmung
KW  - Laminarprofil
KW  - RaWid
KW  - hybrid laminar flow
KW  - suction systems
KW  - suction structure
KW  - contamination
KW  - operational aspects
Y1  - 2000
ER  -