Info
- Utilizzare la checkbox di selezione a fianco di ciascun documento per attivare le funzionalità di stampa, invio email, download nei formati disponibili del (i) record.
Aerodynamic characteristics of 24 NACA 16-series airfoils at Mach numbers between 0.3 and 0.8 / / by W.F. Lindsey, D.B. Stevenson, and Bernard N. Daley
| Aerodynamic characteristics of 24 NACA 16-series airfoils at Mach numbers between 0.3 and 0.8 / / by W.F. Lindsey, D.B. Stevenson, and Bernard N. Daley |
| Autore | Lindsey W. F. |
| Pubbl/distr/stampa | Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1948 |
| Descrizione fisica | 1 online resource (86 pages) : illustrations |
| Collana | Technical notes / National Advisory Committee for Aeronautics |
| Soggetto topico |
Aerodynamics
Aerofoils Wind tunnel testing |
| Formato | Materiale a stampa  |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Altri titoli varianti | Aerodynamic characteristics of twenty four National Advisory Committee for Aeronautics 16-series airfoils at Mach numbers between 0.3 and 0.8 |
| Record Nr. | UNINA-9910713764203321 |
Lindsey W. F.
|
||
| Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1948 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Aerodynamic characteristics of a circular cylinder at Mach number 6.86 and angles of attack up to 90° / / by Jim A. Penland
| Aerodynamic characteristics of a circular cylinder at Mach number 6.86 and angles of attack up to 90° / / by Jim A. Penland |
| Autore | Penland Jim A. |
| Pubbl/distr/stampa | Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1957 |
| Descrizione fisica | 1 online resource (32 pages) : illustrations |
| Collana | Technical notes / National Advisory Committee for Aeronautics |
| Soggetto topico |
Cylinders - Aerodynamics
Aerodynamic load Wind tunnel testing Hypersonic wind tunnels |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Altri titoli varianti | Aerodynamic characteristics of a circular cylinder at Mach number 6.86 and angles of attack up to ninety degrees |
| Record Nr. | UNINA-9910713872803321 |
|
Penland Jim A.
|
||
| Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1957 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
The aerodynamic characteristics of a model wing having a split flap deflected downward and moved to the rear / / by Fred E. Weick and Thomas A. Harris
| The aerodynamic characteristics of a model wing having a split flap deflected downward and moved to the rear / / by Fred E. Weick and Thomas A. Harris |
| Autore | Weick Fred E. |
| Pubbl/distr/stampa | Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1932 |
| Descrizione fisica | 1 online resource (7 pages, 11 unnumbered pages) : illustrations |
| Collana | Technical notes / National Advisory Committee for Aeronautics |
| Soggetto topico |
Wind tunnel testing
Split flaps (Airplanes) Airplanes - Models - Wings Trailing edge flaps |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910713650303321 |
|
Weick Fred E.
|
||
| Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1932 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Aerodynamic characteristics of a two-blade NACA 10-(3)(062)-045 propeller and of a two-blade NACA 10-(3)(08)-045 propeller / / by William Solomon
| Aerodynamic characteristics of a two-blade NACA 10-(3)(062)-045 propeller and of a two-blade NACA 10-(3)(08)-045 propeller / / by William Solomon |
| Autore | Solomon William |
| Pubbl/distr/stampa | Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1953 |
| Descrizione fisica | 1 online resource (53 pages) : illustrations |
| Collana | Technical notes / National Advisory Committee for Aeronautics |
| Soggetto topico |
Propellers, Aerial
Wind tunnel testing Aerodynamics |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Altri titoli varianti | Aerodynamic characteristics of a two-blade NACA 10- |
| Record Nr. | UNINA-9910713893603321 |
|
Solomon William
|
||
| Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1953 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
The aerodynamic characteristics of airfoils as affected by surface roughness / / by Ray W. Hooker
| The aerodynamic characteristics of airfoils as affected by surface roughness / / by Ray W. Hooker |
| Autore | Hooker Ray W. |
| Pubbl/distr/stampa | Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1933 |
| Descrizione fisica | 1 online resource (10 pages, 10 unnumbered pages) : illustrations |
| Collana | Technical notes / National Advisory Committee for Aeronautics |
| Soggetto topico |
Wind tunnel testing
Surface roughness Lift (Aerodynamics) Drag (Aerodynamics) |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910713854803321 |
|
Hooker Ray W.
|
||
| Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1933 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
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.
|
||
| [Washington, D.C.] : , : National Advisory Committee for Aeronautics, , 1932 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
The aerodynamic characteristics of an aspect-ratio-20 wing having thick airfoil sections and employing boundary-layer control by suction / / by Bennie W. Cocke, Jr., Marvin P. Fink, and Stanley M. Gottlieb
| The aerodynamic characteristics of an aspect-ratio-20 wing having thick airfoil sections and employing boundary-layer control by suction / / by Bennie W. Cocke, Jr., Marvin P. Fink, and Stanley M. Gottlieb |
| Autore | Cocke Bennie W. |
| Pubbl/distr/stampa | Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1953 |
| Descrizione fisica | 1 online resource (63 pages) : illustrations |
| Collana | Technical notes / National Advisory Committee for Aeronautics |
| Soggetto topico |
Airplanes - Models - Wings
Aerofoils Boundary layer control Lift (Aerodynamics) Wind tunnel testing |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910713889103321 |
|
Cocke Bennie W.
|
||
| Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1953 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
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 | ||
| ||
The aerodynamic characteristics of three tapered airfoils tested in the variable density wind tunnel / / by Raymond F. Anderson
| The aerodynamic characteristics of three tapered airfoils tested in the variable density wind tunnel / / by Raymond F. Anderson |
| Autore | Anderson Raymond F. |
| Pubbl/distr/stampa | Washington [D.C.] : , : National Advisory Committee for Aeronautics, , 1931 |
| Descrizione fisica | 1 online resource (12 pages, 10 unnumbered pages) : illustrations |
| Collana | Technical notes / National Advisory Committee for Aeronautics |
| Soggetto topico |
Wind tunnel testing
Aerofoils Lift (Aerodynamics) Drag (Aerodynamics) Moments of inertia |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910713651903321 |
|
Anderson Raymond F.
|
||
| Washington [D.C.] : , : National Advisory Committee for Aeronautics, , 1931 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
The aerodynamic design of high Mach number nozzles utilizing axisymmetric flow with application to a nozzle of square test section / / by Ivan E. Beckwith, Herbert W. Ridyard, and Nancy Cromer
| The aerodynamic design of high Mach number nozzles utilizing axisymmetric flow with application to a nozzle of square test section / / by Ivan E. Beckwith, Herbert W. Ridyard, and Nancy Cromer |
| Autore | Beckwith Ivan E. |
| Pubbl/distr/stampa | Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1952 |
| Descrizione fisica | 1 online resource (30 pages) : illustrations |
| Collana | Technical notes / National Advisory Committee for Aeronautics |
| Soggetto topico |
Nozzles - Fluid dynamics
Supersonic nozzles - Design and construction Axial flow Wind tunnel testing Mathematical analysis |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910713895903321 |
|
Beckwith Ivan E.
|
||
| Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1952 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Soggetto topico
-
Wind tunnel testing
(167)
- Aerofoils (36)
- Drag (Aerodynamics) (28)
- Flaps (Airplanes) (25)
- Airplanes - Wings - Testing (24)