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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.  
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
Penland Jim A.  
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
Loftin Laurence K.  
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
Love Eugene S.  
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
Kelly John A.  
Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1954
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui
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
Spreiter John R.  
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
Chapman Dean R.  
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
Pinkerton Robert M.  
Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1930
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui
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
Snyder Melvin H., Jr, <1921->  
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
Ning N. A.  
Golden, CO : , : National Renewable Energy Laboratory, , 2013
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui