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Aerodynamic characteristics at Reynolds numbers of 3.0 x 10⁶ and 6.0 x 10⁶ of three airfoil sections formed by cutting off various amounts from the rear portion of the NACA 0012 airfoil section / / by Hamilton A. Smith and Raymond F. Schaefer
Aerodynamic characteristics at Reynolds numbers of 3.0 x 10⁶ and 6.0 x 10⁶ of three airfoil sections formed by cutting off various amounts from the rear portion of the NACA 0012 airfoil section / / by Hamilton A. Smith and Raymond F. Schaefer
Autore Smith Hamilton A.
Pubbl/distr/stampa Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1950
Descrizione fisica 1 online resource (18 pages) : illustrations
Collana Technical notes / National Advisory Committee for Aeronautics
Soggetto topico Aerofoils
Aerodynamics
Lift (Aerodynamics)
Drag (Aerodynamics)
Pitching (Aerodynamics)
Reynolds number
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Altri titoli varianti Aerodynamic characteristics at Reynolds numbers of 3.0 x 10(exp 6) and 6.0 x 10(exp 6) of three airfoil sections formed by cutting off various amounts from the rear portion of the National Advisory Committee for Aeronautics 0012 airfoil section
Record Nr. UNINA-9910713757103321
Smith Hamilton A.  
Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1950
Materiale a stampa
Lo trovi qui: Univ. Federico II
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Aerodynamic characteristics of a number of modified NACA four-digit-series airfoil sections / / by Laurence K. Loftin, Jr. and Kenneth S. Cohen
Aerodynamic characteristics of a number of modified NACA four-digit-series airfoil sections / / by Laurence K. Loftin, Jr. and Kenneth S. Cohen
Autore Loftin Laurence K.
Pubbl/distr/stampa Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1948
Descrizione fisica 1 online resource (37 pages) : illustrations
Collana Technical notes / National Advisory Committee for Aeronautics
Soggetto topico Aerofoils
Aerodynamics
Flaps (Airplanes)
Aerodynamic load
Lift (Aerodynamics)
Drag (Aerodynamics)
Pitching (Aerodynamics)
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Altri titoli varianti Aerodynamic characteristics of a number of modified National Advisory Committee for Aeronautics four-digit-series airfoil sections
Record Nr. UNINA-9910713763603321
Loftin Laurence K.  
Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1948
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui
Aerodynamic characteristics of the NACA 8-H-12 airfoil section at six Reynolds numbers from 1.8 x 10⁶ to 11.0 x 10⁶ / / by Raymond F. Schaefer and Hamilton A. Smith
Aerodynamic characteristics of the NACA 8-H-12 airfoil section at six Reynolds numbers from 1.8 x 10⁶ to 11.0 x 10⁶ / / by Raymond F. Schaefer and Hamilton A. Smith
Autore Schaefer Raymond F.
Pubbl/distr/stampa Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1949
Descrizione fisica 1 online resource (12 pages) : illustrations
Collana Technical notes / National Advisory Committee for Aeronautics
Soggetto topico Aerofoils
Aerodynamics
Lift (Aerodynamics)
Drag (Aerodynamics)
Pitching (Aerodynamics)
Wind tunnel testing
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Altri titoli varianti Aerodynamic characteristics of the National Advisory Committee for Aeronautics 8-H-12 airfoil section at six Reynolds numbers from 1.8 x 10(exp 6) to 11.0 x 10(exp 6)
Record Nr. UNINA-9910713762303321
Schaefer Raymond F.  
Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1949
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui
Aerodynamic coefficients for an oscillating airfoil with hinged flap, with tables for a Mach number of 0.7 / / by M. J. Turner and S. Rabinowitz
Aerodynamic coefficients for an oscillating airfoil with hinged flap, with tables for a Mach number of 0.7 / / by M. J. Turner and S. Rabinowitz
Autore Turner M. J.
Pubbl/distr/stampa Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1950
Descrizione fisica 1 online resource (46 pages) : illustrations
Collana Technical notes / National Advisory Committee for Aeronautics
Soggetto topico Aerofoils
Flaps (Airplanes)
Lift (Aerodynamics)
Pitching (Aerodynamics)
Hinge moments (Aerodynamics)
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910715016403321
Turner M. J.  
Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1950
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui
Aerodynamic effects caused by icing of an unswept NACA 65A004 airfoil / / by Vernon H. Gray and Uwe H. von Glahn
Aerodynamic effects caused by icing of an unswept NACA 65A004 airfoil / / by Vernon H. Gray and Uwe H. von Glahn
Autore Gray Vernon H.
Pubbl/distr/stampa Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1958
Descrizione fisica 1 online resource (47 pages) : illustrations
Collana Technical notes / National Advisory Committee for Aeronautics
Soggetto topico Aerofoils
Airplanes - Ice prevention
Drag (Aerodynamics)
Leading edges (Aerodynamics)
Lift (Aerodynamics)
Pitching (Aerodynamics)
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Altri titoli varianti Aerodynamic effects caused by icing of an unswept National Advisory Committee for Aeronautics 65A004 airfoil
Record Nr. UNINA-9910713871503321
Gray Vernon H.  
Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1958
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui
Application of the leading-edge-suction analogy to prediction of longitudinal load distribution and pitching moments for sharp-edged delta wings / / by Melvin H. Snyder, Jr., and John E. Lamar
Application of the leading-edge-suction analogy to prediction of longitudinal load distribution and pitching moments for sharp-edged delta wings / / by Melvin H. Snyder, Jr., and John E. Lamar
Autore Snyder Melvin H., Jr, <1921->
Pubbl/distr/stampa Washington, D.C. : , : National Aeronautics and Space Administration, , October 1972
Descrizione fisica 1 online resource (20 pages) : illustrations
Collana NASA/TN
Soggetto topico Aerodynamic loads
Delta wings
Pitching (Aerodynamics)
Airplanes - Wings, Triangular
Vortex-motion
Aerodynamic load
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910716551403321
Snyder Melvin H., Jr, <1921->  
Washington, D.C. : , : National Aeronautics and Space Administration, , October 1972
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui
Board meeting presentations, February 26, 2004 [[electronic resource] ] : Air Midwest flight 5481
Board meeting presentations, February 26, 2004 [[electronic resource] ] : Air Midwest flight 5481
Pubbl/distr/stampa [Washington, D.C.] : , : National Transportation Safety Board, , [2004]
Descrizione fisica 1 electronic document : HTML, digital, Powerpoint, PDF, 3 streaming WMV files
Collana [Accident animations]
Soggetto topico Aircraft accidents - North Carolina - Charlotte
Pitching (Aerodynamics)
Beechcraft (Airplanes) - Performance
Beechcraft (Airplanes) - Accidents
Airplanes - Takeoff - North Carolina - Charlotte
Airplanes - North Carolina - Charlotte - Maintenance and repair
Soggetto genere / forma Animated films.
Streaming videos.
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Nota di contenuto Accident overview: Flight path animation (1 min., 44 secs., WMV file, 4 Mb., sil., col.) -- Pitch control cable system animation (1 min., 39 secs., WMV file, 3.2 Mb., sd., col.) -- Aircraft systems engineering: Pitch control cable system animation (6 min., 27 secs., WMV file, 2.9 Mb., sd., col.) -- Airplane performance -- Aircraft maintenance and records -- Human performance.
Altri titoli varianti Board meeting presentations, February 26, 2004
Record Nr. UNINA-9910697951303321
[Washington, D.C.] : , : National Transportation Safety Board, , [2004]
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui
Static investigation of two STOL nozzle concepts with pitch thrust-vectoring capability / / Mary L. Mason and James R. Burley II
Static investigation of two STOL nozzle concepts with pitch thrust-vectoring capability / / Mary L. Mason and James R. Burley II
Autore Mason Mary L.
Pubbl/distr/stampa Washington, D.C. : , : National Aeronautics and Space Administration, Scientific and Technical Information Branch, , April 1986
Descrizione fisica 1 online resource (54 pages) : illustrations
Collana NASA/TP
Soggetto topico Nozzle geometry
Static tests
Nozzle thrust coefficients
Axisymmetric flow
Afterburning
Jet nozzles - Testing
Airplanes - Motors - Thrust
Pitching (Aerodynamics)
Short take-off and landing aircraft
Soggetto genere / forma Online resources.
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910709724803321
Mason Mary L.  
Washington, D.C. : , : National Aeronautics and Space Administration, Scientific and Technical Information Branch, , April 1986
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui
A study of the pitching moments and the stability characteristics of monoplanes / / by George J. Higgins
A study of the pitching moments and the stability characteristics of monoplanes / / by George J. Higgins
Autore Higgins George J.
Pubbl/distr/stampa Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1934
Descrizione fisica 1 online resource (16 pages, 9 unnumbered pages) : illustrations
Collana Technical note / National Advisory Committee for Aeronautics
Soggetto topico Stability of airplanes
Pitching (Aerodynamics)
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910715921603321
Higgins George J.  
Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1934
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui

Data di pubblicazione