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| 1 |
Improving wing aeroelastic characteristics using periodic design
Badran, Hossam T.;Tawfik, Mohammad;Negm, Hani M.;
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Techno-Press
, v.4, no.4, pp.353-369,
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| 2 |
The feasible constant speed helical trajectories for propeller driven airplanes
Labonte, Gilles;
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Techno-Press
, v.4, no.4, pp.371-399,
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| 3 |
Further results on the development of a novel VTOL aircraft, the Anuloid. Part I: Aerodynamics
Petrolo, Marco;Carrera, Erasmo;Iuso, Gaetano;Patek, Zdenek;Janda, Zdenek;
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Techno-Press
, v.4, no.4, pp.401-419,
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| 4 |
Further results on the development of a novel VTOL aircraft, the Anuloid. Part II: Flight mechanics
Petrolo, Marco;Carrera, Erasmo;Visser, Coen de;D'Ottavio, Michele;Polit, Olivier;
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Techno-Press
, v.4, no.4, pp.421-436,
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| 5 |
Analysis of payload compartment venting of satellite launch vehicle
Mehta, R.C.;
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Techno-Press
, v.4, no.4, pp.437-448,
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| 6 |
Non-linear aero-elastic response of a multi-layer TPS
Pasolini, P.;Dowell, E.H.;Rosa, S. De;Franco, F.;Savino, R.;
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Techno-Press
, v.4, no.4, pp.449-465,
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| 7 |
A multilevel framework for decomposition-based reliability shape and size optimization
Tamijani, Ali Y.;Mulani, Sameer B.;Kapania, Rakesh K.;
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Techno-Press
, v.4, no.4, pp.467-486,
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| 8 |
Effect of geometrical parameters of reentry capsule over flowfield at high speed flow
Mehta, R.C.;
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Techno-Press
, v.4, no.4, pp.487-501,
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