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The aerodynamic characteristics of airfoils at negative angles of attack / / Raymond F. Anderson
| The aerodynamic characteristics of airfoils at negative angles of attack / / Raymond F. Anderson |
| Autore | Anderson Raymond F. |
| Pubbl/distr/stampa | [Washington, D.C.] : , : National Advisory Committee for Aeronautics, , 1932 |
| Descrizione fisica | 1 online resource (11 pages, 26 unnumbered pages) : illustrations |
| Collana | Technical notes / National Advisory Committee for Aeronautics |
| Soggetto topico |
Angle of attack (Aerodynamics)
Wind tunnel testing Aerofoils |
| Formato | Materiale a stampa  |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910713651403321 |
Anderson Raymond F.
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| [Washington, D.C.] : , : National Advisory Committee for Aeronautics, , 1932 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Aerodynamic characteristics of NACA 0012 airfoil section at angles of attack from 0° to 180° / / by Chris C. Critzos, Harry H. Heyson, and Robert W. Boswinkle, Jr
| Aerodynamic characteristics of NACA 0012 airfoil section at angles of attack from 0° to 180° / / by Chris C. Critzos, Harry H. Heyson, and Robert W. Boswinkle, Jr |
| Autore | Critzos Chris C. |
| Pubbl/distr/stampa | Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1955 |
| Descrizione fisica | 1 online resource (21 pages) : illustrations |
| Collana | Technical notes / National Advisory Committee for Aeronautics |
| Soggetto topico |
Aerofoils
Angle of attack (Aerodynamics) Lift (Aerodynamics) |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Altri titoli varianti | Aerodynamic characteristics of National Advisory Committee for Aeronautics 0012 airfoil section at angles of attack from 0 degrees to 180 degrees |
| Record Nr. | UNINA-9910713885603321 |
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Critzos Chris C.
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| Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1955 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Aerodynamic characteristics of several 6-percent-thick airfoils at angles of attack from 0° to 20° at high subsonic speeds / / by Bernard N. Daley and Douglas R. Lord
| Aerodynamic characteristics of several 6-percent-thick airfoils at angles of attack from 0° to 20° at high subsonic speeds / / by Bernard N. Daley and Douglas R. Lord |
| Autore | Daley Bernard N. |
| Pubbl/distr/stampa | Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1955 |
| Descrizione fisica | 1 online resource (57 pages) : illustrations |
| Collana | Technical notes / National Advisory Committee for Aeronautics |
| Soggetto topico |
Aerofoils - Testing
Angle of attack (Aerodynamics) |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Altri titoli varianti | Aerodynamic characteristics of several six-percent-thick airfoils at angles of attack from zero degrees to twenty degrees at high subsonic speeds |
| Record Nr. | UNINA-9910713882603321 |
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Daley Bernard N.
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| Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1955 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Aerodynamic investigation of a four-blade propeller operating through an angle-of-attack range from 0° to 180° / / by H. Clyde McLemore and Michael D. Cannon
| Aerodynamic investigation of a four-blade propeller operating through an angle-of-attack range from 0° to 180° / / by H. Clyde McLemore and Michael D. Cannon |
| Autore | McLemore H. Clyde |
| Pubbl/distr/stampa | Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1954 |
| Descrizione fisica | 1 online resource (62 pages) : illustrations |
| Collana | Technical notes / National Advisory Committee for Aeronautics |
| Soggetto topico |
Angle of attack (Aerodynamics)
Mathematical analysis Propellers, Aerial - Testing Wind tunnel testing |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Altri titoli varianti | Aerodynamic investigation of a four-blade propeller operating through an angle-of-attack range from 0 degrees to 180 degrees |
| Record Nr. | UNINA-9910713887703321 |
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McLemore H. Clyde
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| Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1954 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Aerodynamics of a rectangular wing of infinite aspect ratio at high angles of attack and supersonic speeds / / by John C. Martin and Frank S. Malvestuto, Jr
| Aerodynamics of a rectangular wing of infinite aspect ratio at high angles of attack and supersonic speeds / / by John C. Martin and Frank S. Malvestuto, Jr |
| Autore | Martin John C. |
| Pubbl/distr/stampa | Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1955 |
| Descrizione fisica | 1 online resource (114 pages) : illustrations |
| Collana | Technical notes / National Advisory Committee for Aeronautics |
| Soggetto topico |
Aerodynamics
Aerofoils Airplanes - Wings Angle of attack (Aerodynamics) Aspect ratio (Aerofoils) |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910713882803321 |
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Martin John C.
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| Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1955 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Aerothermal tests of a 12.5° cone at Mach 6.7 for various Reynolds numbers, angles of attack, and nose shapes / / Robert J. Nowak, Cindy W. Albertson, and L. Roane Hunt
| Aerothermal tests of a 12.5° cone at Mach 6.7 for various Reynolds numbers, angles of attack, and nose shapes / / Robert J. Nowak, Cindy W. Albertson, and L. Roane Hunt |
| Autore | Nowak Robert J. |
| Pubbl/distr/stampa | Washington, D.C. : , : National Aeronautics and Space Administration, Scientific and Technical Information Branch, , January 1985 |
| Descrizione fisica | 1 online resource (87 pages) : illustrations |
| Collana | NASA/TP |
| Soggetto topico |
Flow distribution
Cones Aerodynamic heating Boundary layer transition Turbulent boundary layer Angle of attack (Aerodynamics) Noses (Aircraft) Reynolds number Aerothermodynamics |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910709616703321 |
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Nowak Robert J.
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| Washington, D.C. : , : National Aeronautics and Space Administration, Scientific and Technical Information Branch, , January 1985 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Airfoil section characteristics at high angles of attack / / by Laurence K. Loftin, Jr
| Airfoil section characteristics at high angles of attack / / by Laurence K. Loftin, Jr |
| Autore | Loftin Laurence K. |
| Pubbl/distr/stampa | Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1954 |
| Descrizione fisica | 1 online resource (10 pages) : illustrations |
| Collana | Technical notes / National Advisory Committee for Aeronautics |
| Soggetto topico |
Aerofoils
Angle of attack (Aerodynamics) Lift (Aerodynamics) Mach number Reynolds number Surface roughness |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910713887603321 |
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Loftin Laurence K.
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| Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1954 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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An approximate method for pitch-damping prediction [[electronic resource] /] / James E. Danberg and Paul Weinacht
| An approximate method for pitch-damping prediction [[electronic resource] /] / James E. Danberg and Paul Weinacht |
| Autore | Danberg James E |
| Pubbl/distr/stampa | Aberdeen Proving Ground, MD : , : Army Research Laboratory, , [2003] |
| Descrizione fisica | 1 online resource (1 volumes (various pagings)) : digital, PDF file |
| Altri autori (Persone) | WeinachtP |
| Collana | ARL-TR |
| Soggetto topico |
Axial flow
Angle of attack (Aerodynamics) Flight control |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910697248103321 |
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Danberg James E
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| Aberdeen Proving Ground, MD : , : Army Research Laboratory, , [2003] | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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The determination of the angles of attack of zero lift and of zero moment, based on Munk's integrals / / by Max M. Munk
| The determination of the angles of attack of zero lift and of zero moment, based on Munk's integrals / / by Max M. Munk |
| Autore | Munk Max M (Max Michael), <1890-> |
| Pubbl/distr/stampa | [Washington, D.C.] : , : National Advisory Committee for Aeronautics, , 1923 |
| Descrizione fisica | 1 online resource (9 pages, 2 unnumbered pages) : illustrations |
| Collana | Technical notes / National Advisory Committee for Aeronautics |
| Soggetto topico |
Lift (Aerodynamics)
Angle of attack (Aerodynamics) Aerofoils Camber (Aerofoils) |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910713358403321 |
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Munk Max M (Max Michael), <1890->
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| [Washington, D.C.] : , : National Advisory Committee for Aeronautics, , 1923 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Effect of unit Reynolds number, nose bluntness, angle of attack, and roughness on transition on a 5° half-angle cone at Mach 8 / / by P. Calvin Stainback
| Effect of unit Reynolds number, nose bluntness, angle of attack, and roughness on transition on a 5° half-angle cone at Mach 8 / / by P. Calvin Stainback |
| Autore | Stainback P. Calvin |
| Pubbl/distr/stampa | Washington, D.C. : , : National Aeronautics and Space Administration, , January 1969 |
| Descrizione fisica | 1 online resource (76 pages) : illustrations |
| Collana | NASA/TN |
| Soggetto topico |
Reynolds number
Aerodynamics Mach number Aerodynamics, Hypersonic Angle of attack (Aerodynamics) Noses (Space vehicles) |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910716080803321 |
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Stainback P. Calvin
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| Washington, D.C. : , : National Aeronautics and Space Administration, , January 1969 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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