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The aerodynamic drag of five models of side floats, N.A.C.A. models 51-E, 51-F, 51-G, 51-H, and 51-J / / by R.O. House
| The aerodynamic drag of five models of side floats, N.A.C.A. models 51-E, 51-F, 51-G, 51-H, and 51-J / / by R.O. House |
| Autore | House R. O. |
| Pubbl/distr/stampa | Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1938 |
| Descrizione fisica | 1 online resource (6 pages, 3 unnumbered pages) : illustrations |
| Collana | Technical notes / National Advisory Committee for Aeronautics |
| Soggetto topico |
Seaplanes
Pontoons - Aerodynamics Drag (Aerodynamics) |
| Formato | Materiale a stampa  |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Altri titoli varianti | Aerodynamic drag of five models of side floats, National Advisory Committee for Aeronautics models 51-E, 51-F, 51-G, 51-H, and 51-J |
| Record Nr. | UNINA-9910713641103321 |
House R. O.
|
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| Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1938 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
The effects of partial-span plain flaps on the aerodynamic characteristics of a rectangular and a tapered Clark Y-wing / / by R.O. House
| The effects of partial-span plain flaps on the aerodynamic characteristics of a rectangular and a tapered Clark Y-wing / / by R.O. House |
| Autore | House R. O. |
| Pubbl/distr/stampa | Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1938 |
| Descrizione fisica | 1 online resource (6 pages, 7 unnumbered pages) : illustrations |
| Collana | Technical note / National Advisory Committee for Aeronautics |
| Soggetto topico |
Airplanes - Models - Wings
Flaps (Airplanes) Ailerons Wind tunnel testing |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910716849703321 |
|
House R. O.
|
||
| Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1938 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
The effects of partial-span slotted flaps on the aerodynamic characteristics of a rectangular and a tapered N.A.C.A. 23012 wing / / by Rufus O. House
| The effects of partial-span slotted flaps on the aerodynamic characteristics of a rectangular and a tapered N.A.C.A. 23012 wing / / by Rufus O. House |
| Autore | House R. O. |
| Pubbl/distr/stampa | Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1939 |
| Descrizione fisica | 1 online resource (5 pages, 5 unnumbered pages) : illustrations |
| Collana | Technical note / National Advisory Committee for Aeronautics |
| Soggetto topico |
Airplanes - Models - Wings
Slotted flaps (Airplanes) Flaps (Airplanes) Aerodynamics Wind tunnel testing |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910717166803321 |
|
House R. O.
|
||
| Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1939 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Tests of an N.A.C.A. 23012 airfoil with a slotted deflector flap / / by R.O. House
| Tests of an N.A.C.A. 23012 airfoil with a slotted deflector flap / / by R.O. House |
| Autore | House R. O. |
| Pubbl/distr/stampa | Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1939 |
| Descrizione fisica | 1 online resource (5 pages, 3 unnumbered pages) : illustrations |
| Collana | Technical note / National Advisory Committee for Aeronautics |
| Soggetto topico |
Flaps (Airplanes)
Slotted flaps (Airplanes) Aerofoils Wind tunnel testing |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Altri titoli varianti | Tests of an National Advisory Committee for Aeronautics 23012 airfoil with a slotted deflector flap |
| Record Nr. | UNINA-9910716922303321 |
|
House R. O.
|
||
| Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1939 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||