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A method for calculating the aerodynamic loading on wing-body combinations at small angles of attack in supersonic flow / / by Charles M. Jackson, Jr. and Wallace C. Sawyer
| A method for calculating the aerodynamic loading on wing-body combinations at small angles of attack in supersonic flow / / by Charles M. Jackson, Jr. and Wallace C. Sawyer |
| Autore | Jackson Charlie M. |
| Pubbl/distr/stampa | Washington, D.C. : , : National Aeronautics and Space Administration, , October 1971 |
| Descrizione fisica | 1 online resource (32 pages) : illustrations |
| Collana | NASA/TN |
| Soggetto topico |
Aerodynamics
Interference Aerodynamics, Supersonic Interference (Aerodynamics) |
| Formato | Materiale a stampa  |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910715360203321 |
Jackson Charlie M.
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| Washington, D.C. : , : National Aeronautics and Space Administration, , October 1971 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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A method for determining surface pressures on blunt bodies of revolution at small angles of attack in supersonic flow / / by Charlie M. Jackson, Jr., Wallace C. Sawyer, and Rudeen S. Smith
| A method for determining surface pressures on blunt bodies of revolution at small angles of attack in supersonic flow / / by Charlie M. Jackson, Jr., Wallace C. Sawyer, and Rudeen S. Smith |
| Autore | Jackson Charlie M. |
| Pubbl/distr/stampa | Washington, D.C. : , : National Aeronautics and Space Administration, , November 1968 |
| Descrizione fisica | 1 online resource (102 pages) : illustrations |
| Collana | NASA technical note |
| Soggetto topico |
Aerodynamic load
Noses (Space vehicles) - Testing Angle of attack (Aerodynamics) Aerodynamics, Supersonic - Testing |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910714077203321 |
|
Jackson Charlie M.
|
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| Washington, D.C. : , : National Aeronautics and Space Administration, , November 1968 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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A method for determining the total drag of a pointed body of revolution in supersonic flow with turbulent boundary layer / / by Charlie M. Jackson, Jr., and Rudeen S. Smith
| A method for determining the total drag of a pointed body of revolution in supersonic flow with turbulent boundary layer / / by Charlie M. Jackson, Jr., and Rudeen S. Smith |
| Autore | Jackson Charlie M. |
| Pubbl/distr/stampa | Washington, D.C. : , : National Aeronautics and Space Administration, , March 1969 |
| Descrizione fisica | 1 online resource (65 pages) : illustrations |
| Collana | NASA technical note |
| Soggetto topico |
Drag (Aerodynamics)
Boundary layer |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910714087003321 |
|
Jackson Charlie M.
|
||
| Washington, D.C. : , : National Aeronautics and Space Administration, , March 1969 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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