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Accuracy of approximate methods for predicting pressures on pointed nonlifting bodies of revolution in supersonic flow / / by Dorris M. Ehret
| Accuracy of approximate methods for predicting pressures on pointed nonlifting bodies of revolution in supersonic flow / / by Dorris M. Ehret |
| Autore | Ehret Dorris M. |
| Pubbl/distr/stampa | Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1952 |
| Descrizione fisica | 1 online resource (26 pages) : illustrations |
| Collana | Technical notes / National Advisory Committee for Aeronautics |
| Soggetto topico |
Aerodynamics, Supersonic
Aerodynamic load Body of revolution Mathematics |
| Formato | Materiale a stampa  |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910713894503321 |
Ehret Dorris M.
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| Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1952 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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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 |
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Penland Jim A.
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| Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1957 | ||
| 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 |
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Loftin Laurence K.
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| Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1948 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Aerodynamic investigation of a parabolic body of revolution at Mach number of 1.92 and some effects of an annular supersonic jet exhausting from the base / / by Eugene S. Love
| Aerodynamic investigation of a parabolic body of revolution at Mach number of 1.92 and some effects of an annular supersonic jet exhausting from the base / / by Eugene S. Love |
| Autore | Love Eugene S. |
| Pubbl/distr/stampa | Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1956 |
| Descrizione fisica | 1 online resource (62 pages) : illustrations |
| Collana | Technical notes / National Advisory Committee for Aeronautics |
| Soggetto topico |
Aerodynamic load
Aerodynamics, Supersonic Body of revolution |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910713877203321 |
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Love Eugene S.
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| Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1956 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Aerodynamic loads on a leading-edge flap and a leading-edge slat on the NACA 64A010 airfoil section / / by John A. Kelly and George B. McCullough
| Aerodynamic loads on a leading-edge flap and a leading-edge slat on the NACA 64A010 airfoil section / / by John A. Kelly and George B. McCullough |
| Autore | Kelly John A. |
| Pubbl/distr/stampa | Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1954 |
| Descrizione fisica | 1 online resource (33 pages) : illustrations |
| Collana | Technical notes / National Advisory Committee for Aeronautics |
| Soggetto topico |
Aerodynamic load
Aerofoils Flaps (Airplanes) Leading edge flaps Leading edges (Aerodynamics) |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Altri titoli varianti | Aerodynamic loads on a leading-edge flap and a leading-edge slat on the National Advisory Committee for Aeronautics 64A010 airfoil section |
| Record Nr. | UNINA-9910713887803321 |
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Kelly John A.
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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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Aerodynamic properties of cruciform-wing and body combinations at subsonic, transonic, and supersonic speeds / / by John R. Spreiter
| Aerodynamic properties of cruciform-wing and body combinations at subsonic, transonic, and supersonic speeds / / by John R. Spreiter |
| Autore | Spreiter John R. |
| Pubbl/distr/stampa | Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1949 |
| Descrizione fisica | 1 online resource (32 pages) : illustrations |
| Collana | Technical notes / National Advisory Committee for Aeronautics |
| Soggetto topico |
Aerodynamic load
Aerodynamics Airplanes - Wings |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910713762903321 |
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Spreiter John R.
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| Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1949 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Airfoil profiles for minimum pressure drag at supersonic velocities - application of shock-expansion theory, including consideration of hypersonic range / / by Dean R. Chapman
| Airfoil profiles for minimum pressure drag at supersonic velocities - application of shock-expansion theory, including consideration of hypersonic range / / by Dean R. Chapman |
| Autore | Chapman Dean R. |
| Pubbl/distr/stampa | Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1952 |
| Descrizione fisica | 1 online resource (44 pages) : illustrations |
| Collana | Technical notes / National Advisory Committee for Aeronautics |
| Soggetto topico |
Aerodynamic load
Aerodynamics, Supersonic Aerofoils Drag (Aerodynamics) |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910713894003321 |
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Chapman Dean R.
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| Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1952 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Analytical determination of the load on a trailing edge flap / / by Robert M. Pinkerton
| Analytical determination of the load on a trailing edge flap / / by Robert M. Pinkerton |
| Autore | Pinkerton Robert M. |
| Pubbl/distr/stampa | Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1930 |
| Descrizione fisica | 1 online resource (7 pages, 2 unnumbered pages) : illustrations |
| Collana | Technical notes / National Advisory Committee for Aeronautics |
| Soggetto topico |
Aeronautics
Aerodynamic load |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910715024503321 |
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Pinkerton Robert M.
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| Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1930 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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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 |
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Snyder Melvin H., Jr, <1921->
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| Washington, D.C. : , : National Aeronautics and Space Administration, , October 1972 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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CCBLADE documentation / / S.A. Ning
| CCBLADE documentation / / S.A. Ning |
| Autore | Ning N. A. |
| Edizione | [Release 0.1.0.] |
| Pubbl/distr/stampa | Golden, CO : , : National Renewable Energy Laboratory, , 2013 |
| Descrizione fisica | 1 online resource (iv, 23 pages) : color illustrations |
| Collana | NREL/TP |
| Soggetto topico |
Turbines - Blades - Computer simulation
Wind turbines - Computer simulation Aerodynamic load |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910703908903321 |
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Ning N. A.
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| Golden, CO : , : National Renewable Energy Laboratory, , 2013 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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