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An approximate axisymmetric viscous shock layer aeroheating method for three-dimensional bodies / / Irina G. Brykina, Carl D. Scott
An approximate axisymmetric viscous shock layer aeroheating method for three-dimensional bodies / / Irina G. Brykina, Carl D. Scott
Autore Brykina Irina G.
Pubbl/distr/stampa Houston, Texas : , : National Aeronautics and Space Administration, Lyndon B. Johnson Space Center, , May 1998
Descrizione fisica 1 online resource (iv, 28 pages) : illustrations
Collana NASA/TM
Soggetto topico Flow measurement
Axisymmetric flow
Aerodynamic heating
Parabolic bodies
Hypersonics
Axisymmetric bodies
Blunt bodies
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910705868703321
Brykina Irina G.  
Houston, Texas : , : National Aeronautics and Space Administration, Lyndon B. Johnson Space Center, , May 1998
Materiale a stampa
Lo trovi qui: Univ. Federico II
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A computer program for systematically analyzing free-flight data to determine the aerodynamics of axisymmetric bodies / / by Gerald N. Malcolm and Gary T. Chapman
A computer program for systematically analyzing free-flight data to determine the aerodynamics of axisymmetric bodies / / by Gerald N. Malcolm and Gary T. Chapman
Autore Malcolm Gerald N.
Pubbl/distr/stampa Washington, D.C. : , : National Aeronautics and Space Administration, , September 1968
Descrizione fisica 1 online resource (37 pages) : illustrations
Collana NASA technical note
Soggetto topico Aerodynamics
Axisymmetric bodies
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910715037803321
Malcolm Gerald N.  
Washington, D.C. : , : National Aeronautics and Space Administration, , September 1968
Materiale a stampa
Lo trovi qui: Univ. Federico II
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An investigation at static conditions of nonaxisymmetric nozzle thrust reverser port geometry including effects of rounding and rotating the port corner [[electronic resource] /] / Dorothy G. Arbiter
An investigation at static conditions of nonaxisymmetric nozzle thrust reverser port geometry including effects of rounding and rotating the port corner [[electronic resource] /] / Dorothy G. Arbiter
Autore Arbiter Dorothy G
Pubbl/distr/stampa Hampton, Va. : , : Vigyan Research Associates, Inc. : , : National Aeronautics and Space Administration, Langley Research Center, , [1985]
Descrizione fisica 1 volume : PDF file
Collana NASA contractor report
Soggetto topico Axisymmetric bodies
Investigation
Nozzle thrust coefficients
Ports (openings)
Rotating cylinders
Static tests
Thrust reversal
Wind tunnel tests
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910699288403321
Arbiter Dorothy G  
Hampton, Va. : , : Vigyan Research Associates, Inc. : , : National Aeronautics and Space Administration, Langley Research Center, , [1985]
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui
Parametric fin-body and fin-plate database for a series of 12 missile fins / / Jerry M. Allen
Parametric fin-body and fin-plate database for a series of 12 missile fins / / Jerry M. Allen
Autore Allen Jerry M.
Pubbl/distr/stampa Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , January 2001
Descrizione fisica 1 online resource (vi, 296 pages) : illustrations
Collana NASA/TM
Soggetto topico Axisymmetric bodies
Data bases
Experimentation
Fins
Flat plates
Soggetto genere / forma Tables.
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910706578903321
Allen Jerry M.  
Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , January 2001
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui
Spin forming of an aluminum 2219-T6 aft bulkhead for the Orion Multi-Purpose Crew Vehicle: phase II supplemental report / / Robert S. Piascik [and three others]
Spin forming of an aluminum 2219-T6 aft bulkhead for the Orion Multi-Purpose Crew Vehicle: phase II supplemental report / / Robert S. Piascik [and three others]
Autore Piascik Robert S.
Pubbl/distr/stampa Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , December 2015
Descrizione fisica 1 online resource (151 pages) : color illustrations
Collana NASA/TM
Soggetto topico Aluminum
Axisymmetric bodies
Crew Exploration Vehicle
Metal spinning
Stress intensity factors
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Altri titoli varianti Spin forming of an aluminum 2219-T6 aft bulkhead for the Orion Multi-Purpose Crew Vehicle
Record Nr. UNINA-9910707116603321
Piascik Robert S.  
Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , December 2015
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui
Static internal performance of single -expansion-ramp nozzles with thrust-vectoring capability up to 60° / / Bobby L. Berrier and Laurence D. Leavitt
Static internal performance of single -expansion-ramp nozzles with thrust-vectoring capability up to 60° / / Bobby L. Berrier and Laurence D. Leavitt
Autore Berrier Bobby L.
Pubbl/distr/stampa [Washington, D.C.] : , : National Aeronautics and Space Administration, Scientific and Technical Information Branch, , October 1984
Descrizione fisica 1 online resource (141 pages) : illustrations
Collana NASA technical paper
Soggetto topico Axisymmetric bodies
Nozzle thrust coefficients
Static tests
Thrust vector control
Transonic wind tunnels
Two dimensional flow
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Altri titoli varianti Static internal performance of single -expansion-ramp nozzles with thrust-vectoring capability up to 60 degrees
Record Nr. UNINA-9910707970903321
Berrier Bobby L.  
[Washington, D.C.] : , : National Aeronautics and Space Administration, Scientific and Technical Information Branch, , October 1984
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui

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