@article{Hillen1980, author = {Hillen, Walter}, title = {K0 production in e+e\&\#8722; annihilations at 30 GeV center of mass energy. TASSO Collaboration}, series = {Physics Letters B. 94 (1980), H. 1}, journal = {Physics Letters B. 94 (1980), H. 1}, isbn = {0370-2693}, pages = {91 -- 95}, year = {1980}, language = {en} } @article{Hillen1980, author = {Hillen, Walter}, title = {Test of QED in e+e\&\#8722; annihilation at energies between 12 and 31.6 GeV. TASSO Collaboration}, series = {Physics Letters B. 94 (1980), H. 2}, journal = {Physics Letters B. 94 (1980), H. 2}, isbn = {0370-2693}, pages = {259 -- 265}, year = {1980}, language = {en} } @article{Hillen1980, author = {Hillen, Walter}, title = {Rapid growth of charged particle multiplicity in high energy e+e\&\#8722; annihilations. TASSO Collaboration}, series = {Physics Letters B. 89 (1980), H. 3-4}, journal = {Physics Letters B. 89 (1980), H. 3-4}, isbn = {0370-2693}, pages = {418 -- 422}, year = {1980}, language = {en} } @article{Hillen1980, author = {Hillen, Walter}, title = {Production and properties of the \&\#964;-lepton in e+e\&\#8722; annihilation at C.M. energies from 12 to 31.6 GeV. TASSO Collaboration}, series = {Physics Letters B. 92 (1980), H. 1-2}, journal = {Physics Letters B. 92 (1980), H. 1-2}, isbn = {0370-2693}, pages = {199 -- 205}, year = {1980}, language = {en} } @article{Hillen1979, author = {Hillen, Walter}, title = {Evidence for planar events in e+e\&\#8722; annihilation at high energies. TASSO Collaboration}, series = {Physics Letters B. 86 (1979), H. 2}, journal = {Physics Letters B. 86 (1979), H. 2}, isbn = {0370-2693}, pages = {243 -- 249}, year = {1979}, language = {en} } @article{Hillen1982, author = {Hillen, Walter}, title = {Charged pion production in e--e+ annihilation at 14, 22 and 34 GeV c.m. energies. TASSO Collaboration}, series = {Physics Letters B. 113 (1982), H. 1}, journal = {Physics Letters B. 113 (1982), H. 1}, isbn = {0370-2693}, pages = {98 -- 104}, year = {1982}, language = {en} } @article{Hillen1982, author = {Hillen, Walter}, title = {Charge asymmetry and weak interaction effects in e+e\&\#8722;\&\#8594;\&\#956;+\&\#956;\&\#8722; and e+e\&\#8722;\&\#8594;\&\#964;+\&\#964;\&\#8722; . TASSO Collaboration}, series = {Physics Letters B. 110 (1982), H. 2}, journal = {Physics Letters B. 110 (1982), H. 2}, isbn = {0370-2693}, pages = {173 -- 180}, year = {1982}, language = {en} } @article{Hillen1982, author = {Hillen, Walter}, title = {\&\#960;0 production by e+e\&\#8722; annihilation at 14 and 34 GeV c.m. energy . TASSO Collaboration}, series = {Physics Letters B. 108 (1982), H. 1}, journal = {Physics Letters B. 108 (1982), H. 1}, isbn = {0370-2693}, pages = {71 -- 76}, year = {1982}, language = {en} } @article{Hillen1982, author = {Hillen, Walter}, title = {Exclusive proton-antiproton production in two photon collisions . TASSO Collaboration}, series = {Physics Letters B. 108 (1982), H. 1}, journal = {Physics Letters B. 108 (1982), H. 1}, isbn = {0370-2693}, pages = {67 -- 70}, year = {1982}, language = {en} } @article{Hillen1982, author = {Hillen, Walter}, title = {High pT hadron production in photon-photon collisions . TASSO Collaboration}, series = {Physics Letters B. 107 (1982), H. 4}, journal = {Physics Letters B. 107 (1982), H. 4}, isbn = {0370-2693}, pages = {290 -- 296}, year = {1982}, language = {en} } @article{Hillen1981, author = {Hillen, Walter}, title = {\&\#923;, Image production in e+e- annihilation at 33 GeV centre of mass energy. TASSO Collaboration}, series = {Physics Letters B. 105 (1981), H. 4}, journal = {Physics Letters B. 105 (1981), H. 4}, isbn = {0370-2693}, pages = {75 -- 80}, year = {1981}, language = {en} } @article{Hillen1981, author = {Hillen, Walter}, title = {Evidence for charged primary partons in e+e\&\#8722; \&\#8594; 2 jets. TASSO Collaboration}, series = {Physics Letters B. 100 (1981), H. 4}, journal = {Physics Letters B. 100 (1981), H. 4}, isbn = {0370-2693}, pages = {357 -- 363}, year = {1981}, language = {en} } @article{Hillen1981, author = {Hillen, Walter}, title = {Search for new sequential leptons in e+e- annihilation at petra energies. TASSO Collaboration}, series = {Physics Letters B. 99 (1981), H. 2}, journal = {Physics Letters B. 99 (1981), H. 2}, isbn = {0370-2693}, pages = {163 -- 168}, year = {1981}, language = {en} } @article{Hillen1980, author = {Hillen, Walter}, title = {Evidence for a spin-1 gluon in three-jet events. TASSO Collaboration}, series = {Physics Letters B. 97 (1980), H. 3-4}, journal = {Physics Letters B. 97 (1980), H. 3-4}, isbn = {0370-2693}, pages = {453 -- 458}, year = {1980}, language = {en} } @article{Hillen1980, author = {Hillen, Walter}, title = {RHO-RHO production by two photon scattering. TASSO Collaboration}, series = {Physics Letters B. 97 (1980), H. 3-4}, journal = {Physics Letters B. 97 (1980), H. 3-4}, isbn = {0370-2693}, pages = {448 -- 452}, year = {1980}, language = {en} } @incollection{Mertens1997, author = {Mertens, Josef}, title = {Aerodynamic multi point design challenge}, series = {New design concepts for high speed air transport.- (Courses and lectures / International Centre for Mechanical Sciences ; 366)}, booktitle = {New design concepts for high speed air transport.- (Courses and lectures / International Centre for Mechanical Sciences ; 366)}, editor = {Sobieczky, H.}, publisher = {Springer}, address = {Wien [u.a.]}, isbn = {3-2118-2815-X}, doi = {10.1007/978-3-7091-2658-5_4}, pages = {53 -- 67}, year = {1997}, abstract = {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.}, language = {en} } @incollection{Mertens1997, author = {Mertens, Josef}, title = {Required aerodynamic technologies}, series = {New design concepts for high speed air transport. - (Courses and lectures / International Centre for Mechanical Sciences ; 366)}, booktitle = {New design concepts for high speed air transport. - (Courses and lectures / International Centre for Mechanical Sciences ; 366)}, editor = {Sobieczky, H.}, publisher = {Springer}, address = {Wien [u.a.]}, isbn = {3-2118-2815-X}, doi = {10.1007/978-3-7091-2658-5_5}, pages = {69 -- 96}, year = {1997}, abstract = {In the preceeding chapters on "Son of Concorde, a Technology Challenge" and "Aerodynamic Multipoint Design Challenge" it was explained, that a well balanced contribution of new technologies in all major disciplines is required for realisation of a new Supersonic Commercial Transport (SCT). One of these technologies - usually one of the most important for aircraft-is aerodynamics. Here, the required "pure" aerodynamic technologies are specified in more detail, according to our present knowledge. Increasing insight into the problems may change the balance of importance of the individual technologies and may require some more contributions. We must never confine our knowledge to the knowledge base of an expert at a given time, but must stay open for new insights.}, language = {en} } @incollection{Mertens1997, author = {Mertens, Josef}, title = {Certification of supersonic civil transports}, series = {New design concepts for high speed air transport. - (Courses and lectures / International Centre for Mechanical Sciences ; 366)}, booktitle = {New design concepts for high speed air transport. - (Courses and lectures / International Centre for Mechanical Sciences ; 366)}, editor = {Sobieczky, H.}, publisher = {Springer}, address = {Wien [u.a.]}, isbn = {3-2118-2815-X}, doi = {10.1007/978-3-7091-2658-5_6}, pages = {97 -- 103}, year = {1997}, abstract = {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].}, language = {en} } @incollection{Mertens1997, author = {Mertens, Josef}, title = {Supersonic laminar flow}, series = {New design concepts for high speed air transport. - (Courses and lectures / International Centre for Mechanical Sciences ; 366)}, booktitle = {New design concepts for high speed air transport. - (Courses and lectures / International Centre for Mechanical Sciences ; 366)}, editor = {Sobieczky, H.}, publisher = {Springer}, address = {Wien [u.a.]}, isbn = {3-2118-2815-X}, doi = {10.1007/978-3-7091-2658-5_18}, pages = {275 -- 290}, year = {1997}, abstract = {Supersonic transports are very drag sensitive. Technology to reduce drag by application of laminar flow, therefore, will be important; it is a prerequisite to achieve very long range capability. In earlier studies it was assumed that SCTs would only become possible by application of laminar flow [376]. But today, we request an SCT to be viable without application of laminar flow in order to maintain its competitiveness when laminar flow becomes available for subsonic and supersonic transports. By reducing fuel burned, laminar flow drag reduction reduces size and weight of the aircraft, or increases range capability -whereas otherwise size and weight would grow towards infinity. Transition mechanisms from laminar to turbulent state of the boundary layer flow (ALT, CFI, TSI) function as for transonic transports, but at more severe conditions: higher sweep angles, cooled surfaces; higher mode instabilities (HMI) must at least be taken into account, although they may not become important below Mach 3. Hitherto there is a worldwide lack of ground test facilities to investigate TSI at the expected cruise Mach numbers between 1.6 and 2.4; in Stuttgart, Germany one such facility -a Ludwieg tube- is still in the validation phase. A quiet Ludwieg tunnel could be a favourable choice for Europe. But it will require a new approach in designing aircraft which includes improved theoretical predictions, usage of classical wind tunnels for turbulent flow and flight tests for validation.}, language = {en} } @incollection{MertensBecker1989, author = {Mertens, Josef and Becker, K.}, title = {Numerical solution of flow equations : an aircraft designer's view}, series = {Nonlinear hyperbolic equations - theory, computation methods, and applications : proceedings of the 2nd International Conference on Nonlinear Hyperbolic Problems, Aachen, FRG, March 14 to 18, 1988. - (Notes on Numerical Fluid Mechanics ; 24)}, booktitle = {Nonlinear hyperbolic equations - theory, computation methods, and applications : proceedings of the 2nd International Conference on Nonlinear Hyperbolic Problems, Aachen, FRG, March 14 to 18, 1988. - (Notes on Numerical Fluid Mechanics ; 24)}, editor = {Ballmann, Josef}, publisher = {Vieweg}, address = {Braunschweig}, isbn = {3-528-08098-1}, doi = {10.1007/978-3-322-87869-4_41}, pages = {403 -- 412}, year = {1989}, abstract = {Today the most accurate and cost effective industrial codes used in aircraft design are based on the full potential equation coupled with boundary layer equations. However, these are not capable to solve complicated three-dimensional problems of vortical flows and shocks. On the other hand Euler and Navier-Stokes codes are too expensive and not accurate enough for design purposes, especially in regard of drag and interference prediction. The reasons for these deficiencies are investigated and a way to overcome them by future developments is demonstrated.}, language = {en} }