Span load distribution on two monoplane wing models as affected by twist and sweepback / / by Montgomery Knight and Richard W. Noyes
| Span load distribution on two monoplane wing models as affected by twist and sweepback / / by Montgomery Knight and Richard W. Noyes |
| Autore | Knight Montgomery |
| Pubbl/distr/stampa | Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1930 |
| Descrizione fisica | 1 online resource (7 pages, 12 unnumbered pages) : illustrations |
| Collana | Technical notes / National Advisory Committee for Aeronautics |
| Soggetto topico |
Airplanes - Models - Wings
Loads (Mechanics) Stability of airplanes |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910714048703321 |
Knight Montgomery
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| Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1930 | ||
| Lo trovi qui: Univ. Federico II | ||
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Wind tunnel pressure distribution tests on a series of biplane wing models . Part II Effects of changes in decalage, dihedral, sweepback and overhang / / by Montgomery Knight and Richard W. Noyes
| Wind tunnel pressure distribution tests on a series of biplane wing models . Part II Effects of changes in decalage, dihedral, sweepback and overhang / / by Montgomery Knight and Richard W. Noyes |
| Autore | Knight Montgomery |
| Pubbl/distr/stampa | Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1929 |
| Descrizione fisica | 1 online resource (6 pages, 32 unnumbered pages) : illustrations |
| Collana | Technical notes / National Advisory Committee for Aeronautics |
| Soggetto topico |
Airplanes - Dihedral wings
Airplanes - Models - Testing Airplanes - Wings, Swept-back Aerodynamic load - Testing Wind tunnel testing Biplanes |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Altri titoli varianti | Effects of changes in decalage, dihedral, sweepback and overhang |
| Record Nr. | UNINA-9910713819203321 |
Knight Montgomery
|
||
| Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1929 | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Wind tunnel pressure distribution tests on a series of biplane wing models . Part III Effects of changes in various combinations of stagger, gap, sweepback, and decalage / / by Montgomery Knight and Richard W. Noyes
| Wind tunnel pressure distribution tests on a series of biplane wing models . Part III Effects of changes in various combinations of stagger, gap, sweepback, and decalage / / by Montgomery Knight and Richard W. Noyes |
| Autore | Knight Montgomery |
| Pubbl/distr/stampa | Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1929 |
| Descrizione fisica | 1 online resource (6 pages, 22 unnumbered pages) : illustrations |
| Collana | Technical notes / National Advisory Committee for Aeronautics |
| Soggetto topico |
Aerodynamic load - Testing
Airplanes - Models - Testing Airplanes - Wings, Swept-back Wind tunnel testing Biplanes |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Altri titoli varianti | Effects of changes in various combinations of stagger, gap, sweepback, and decalage |
| Record Nr. | UNINA-9910713805003321 |
Knight Montgomery
|
||
| Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1929 | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Wind tunnel pressure distribution tests on a series of biplane wing models . Part I Effects of changes in stagger and gap / / by Montgomery Knight and Richard W. Noyes
| Wind tunnel pressure distribution tests on a series of biplane wing models . Part I Effects of changes in stagger and gap / / by Montgomery Knight and Richard W. Noyes |
| Autore | Knight Montgomery |
| Pubbl/distr/stampa | Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1929 |
| Descrizione fisica | 1 online resource (13 pages, 20 unnumbered pages) : illustrations |
| Collana | Technical notes / National Advisory Committee for Aeronautics |
| Soggetto topico |
Airplanes - Wings - Design and construction
Wind tunnel testing Biplanes |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Altri titoli varianti | Effects of changes in stagger and gap |
| Record Nr. | UNINA-9910713862303321 |
Knight Montgomery
|
||
| Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1929 | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Wind-tunnel research comparing lateral control devices, particularly at high angles of attack . X Various control devices on a wing with a fixed auxiliary airfoil / / by Fred E. Weick and Richard W. Noyes
| Wind-tunnel research comparing lateral control devices, particularly at high angles of attack . X Various control devices on a wing with a fixed auxiliary airfoil / / by Fred E. Weick and Richard W. Noyes |
| Autore | Weick Fred E. |
| Pubbl/distr/stampa | Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1933 |
| Descrizione fisica | 1 online resource (18 pages, 9 unnumbered pages) : illustrations |
| Collana | Technical note / National Advisory Committee for Aeronautics |
| Soggetto topico |
Airplanes - Wings - Testing
Airplanes - Control surfaces Spoilers (Airplanes) Wind tunnel testing |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Altri titoli varianti | Various control devices on a wing with a fixed auxiliary airfoil |
| Record Nr. | UNINA-9910715240503321 |
Weick Fred E.
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| Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1933 | ||
| Lo trovi qui: Univ. Federico II | ||
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