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Application of the leading-edge-suction analogy of vortex lift to the drag due to lift of sharp-edge delta wings / / by Edward C. Polhamus
| Application of the leading-edge-suction analogy of vortex lift to the drag due to lift of sharp-edge delta wings / / by Edward C. Polhamus |
| Autore | Polhamus Edward C (Edward Charles), <1923-2001, > |
| Pubbl/distr/stampa | Washington, D.C. : , : National Aeronautics and Space Administration, , August 1968 |
| Descrizione fisica | 1 online resource (14 pages) : illustrations |
| Collana | NASA technical note |
| Soggetto topico |
Delta wing airplanes
Vortex flaps Drag (Aerodynamics) Lift (Aerodynamics) |
| Formato | Materiale a stampa  |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910715018403321 |
Polhamus Edward C (Edward Charles), <1923-2001, >
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| Washington, D.C. : , : National Aeronautics and Space Administration, , August 1968 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Calculation of vortex-flap aerodynamic characteristics / / by C. Edward Lan and C.C. Hsing
| Calculation of vortex-flap aerodynamic characteristics / / by C. Edward Lan and C.C. Hsing |
| Autore | Lan C. Edward (Chuan-Tau Edward), <1935-> |
| Pubbl/distr/stampa | Lawrence, Kansas : , : Flight Research Laboratory, Department of Aerospace Engineering, the University of Kansas |
| Descrizione fisica | 1 online resource (6 pages) : illustrations |
| Collana | NASA-CR |
| Soggetto topico |
Aerodynamic configurations
Angle of attack Leading edges Spline functions Swept wings Vortex breakdown Vortex flaps |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910705290203321 |
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Lan C. Edward (Chuan-Tau Edward), <1935->
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| Lawrence, Kansas : , : Flight Research Laboratory, Department of Aerospace Engineering, the University of Kansas | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Low-speed aerodynamic data for an 0.18-scale model of an F-16XL with various leading-edge modifications / / David E. Hahne
| Low-speed aerodynamic data for an 0.18-scale model of an F-16XL with various leading-edge modifications / / David E. Hahne |
| Autore | Hahne David E (David Edgar) |
| Pubbl/distr/stampa | Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , December 1999 |
| Descrizione fisica | 1 online resource (164 pages) : illustrations |
| Collana | NASA/TM |
| Soggetto topico |
Scale models
Leading edges Data bases F-16 aircraft Leading edge sweep Vortex flaps |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910706119903321 |
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Hahne David E (David Edgar)
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| Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , December 1999 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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VORCOR : a computer program for calculating characteristics of wings with edge vortex separation by using a vortex filament and core model / / Jenn-Louh Pao, Sudhir C. Mehrotra, C. Edward Lan
| VORCOR : a computer program for calculating characteristics of wings with edge vortex separation by using a vortex filament and core model / / Jenn-Louh Pao, Sudhir C. Mehrotra, C. Edward Lan |
| Autore | Pao Jenn-Louh |
| Pubbl/distr/stampa | Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , April 1982 |
| Descrizione fisica | 1 online resource (241 pages, 1 unnumbered page) : illustrations |
| Collana | NASA contractor report |
| Soggetto topico |
Computer programs
Vortex flaps Computerized simulation Aerodynamics Mathematical models |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Altri titoli varianti | VORCOR |
| Record Nr. | UNINA-9910709973703321 |
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Pao Jenn-Louh
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| Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , April 1982 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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