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Wind-tunnel investigation of effect of yaw on lateral-stability characteristics . II Rectangular N.A.C.A. 23012 wing with a circular fuselage and a fin / / by M.J. Bamber and R.O. House



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Autore: Bamber M. J. Visualizza persona
Titolo: Wind-tunnel investigation of effect of yaw on lateral-stability characteristics . II Rectangular N.A.C.A. 23012 wing with a circular fuselage and a fin / / by M.J. Bamber and R.O. House Visualizza cluster
Pubblicazione: Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1939
Descrizione fisica: 1 online resource (9 pages, 11 unnumbered pages) : illustrations
Soggetto topico: Airplanes - Wings - Testing
Airplanes - Fuselage
Stability of airplanes
Rolling (Aerodynamics)
Yawing (Aerodynamics)
Wind tunnel testing
Persona (resp. second.): HouseR. O.
Note generali: "September 1939."
No Federal Depository Library Program (FDLP) item number.
Nota di bibliografia: Includes bibliographical references (page 9).
Altri titoli varianti: Rectangular N.A.C.A. 23012 wing with a circular fuselage and a fin
Rectangular National Advisory Committee for Aeronautics 23012 wing with a circular fuselage and a fin
Titolo autorizzato: Wind-tunnel investigation of effect of yaw on lateral-stability characteristics  Visualizza cluster
Formato: Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione: Inglese
Record Nr.: 9910716912803321
Lo trovi qui: Univ. Federico II
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