An investigation into the vertical axis control power requirements for landing VTOL type aircraft onboard non-aviation ships in various sea states [[electronic resource] /] / prepared by Mark E. Stevens, principal investigator, Jan Roskam |
Autore | Stevens Mark E |
Pubbl/distr/stampa | Lawrence, Kansas : , : Flight Research Laboratory, University of Kansas Center for Research, Inc. |
Descrizione fisica | 1 online resource (xiv, 79 pages, 123 unnumbered pages) : illustrations |
Altri autori (Persone) | RoskamJan |
Collana | NASA-CR |
Soggetto topico |
Aircraft landing
Sea states Ships Simulation Turbulence Vertical takeoff aircraft |
Formato | Materiale a stampa |
Livello bibliografico | Monografia |
Lingua di pubblicazione | eng |
Altri titoli varianti | Vertical axis control power requirements for landing Vertical takeoff and landing Vertical Takeoff and Landing type aircraft onboard non-aviation ships in various sea states |
Record Nr. | UNINA-9910701516303321 |
Stevens Mark E | ||
Lawrence, Kansas : , : Flight Research Laboratory, University of Kansas Center for Research, Inc. | ||
Materiale a stampa | ||
Lo trovi qui: Univ. Federico II | ||
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Propulsion and airframe aerodynamic interactions of supersonic V/STOL configurations, Phase I / / M.R. Mraz, P.E. Hiley |
Autore | Mraz M. R. |
Pubbl/distr/stampa | St. Louis, Missouri : , : McDonnell Aircraft Company |
Descrizione fisica | 1 online resource (xii, 132 pages) : illustrations |
Collana | NASA contractor report |
Soggetto topico |
Aerodynamic interference
Airframes Fighter aircraft Propulsion system configurations Short takeoff aircraft Supersonic aircraft Vertical takeoff aircraft |
Formato | Materiale a stampa |
Livello bibliografico | Monografia |
Lingua di pubblicazione | eng |
Altri titoli varianti | Propulsion and airframe aerodynamic interactions of supersonic V STOL configurations, Phase I |
Record Nr. | UNINA-9910705490303321 |
Mraz M. R. | ||
St. Louis, Missouri : , : McDonnell Aircraft Company | ||
Materiale a stampa | ||
Lo trovi qui: Univ. Federico II | ||
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