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Analysis of A Jet in A Subsonic CrosswindJet exhaust flow effects on aerodynamic characteristics of V/STOL aircraft during transition flight
Document ID
19700002522
Acquisition Source
Headquarters
Document Type
Special Publication (SP)
Date Acquired
September 2, 2013
Publication Date
January 1, 1969
Publication Information
Publisher: National Aeronautics and Space Administration
Subject Category
Aerodynamics
Report/Patent Number
NASA-SP-218
Meeting Information
Meeting: Symposium held at Langley Research Center
Location: Hampton, VA
Country: US
Start Date: September 9, 1969
End Date: September 10, 1969
Sponsors: National Aeronautics and Space Administration
Accession Number
70N11826
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

Related Records

IDRelationTitle19700002523WorkJet-wake characteristics and their induced aerodynamic effects on V/STOL aircraft in transition flight19700002524WorkThe physical nature of the subsonic jet in a cross-stream19700002525WorkThe aerodynamics of the lifting jet in a cross flowing stream19700002526WorkExperimental investigation of pressures induced on a flat plate by a jet issuing into a subsonic crosswind19700002527WorkExperimental reaction jet effects at subsonic speeds19700002528WorkA blockage-sink representation of jet interference effects for noncircular jet orifices19700002529WorkDevelopment of an analytical model for the flow of a jet into a subsonic crosswind19700002530WorkNumerical treatment of line singularities for modelling a jet in a low-speed cross flow19700002531WorkAnalytic description of jet-wake cross sections for a jet normal to a subsonic free stream19700002532WorkCross wind effects on trajectory and cross sections of turbulent jets19700002533WorkA general jet efflux simulation model19700002534WorkCalculation of jet interference effects on V/STOL aircraft by a nonplanar potential flow method19700002535WorkInviscid models for the pressure induced by a jet transverse to a subsonic stream19700002536WorkThe Use of Matched Asymptotic Expansions as an Approach to the Problem of the Jet in A Cross Flow19700002537WorkMass entrainment of a circular jet in a cross flow19700002523WorkJet-wake characteristics and their induced aerodynamic effects on V/STOL aircraft in transition flight19700002524WorkThe physical nature of the subsonic jet in a cross-stream19700002525WorkThe aerodynamics of the lifting jet in a cross flowing stream19700002526WorkExperimental investigation of pressures induced on a flat plate by a jet issuing into a subsonic crosswind19700002527WorkExperimental reaction jet effects at subsonic speeds19700002528WorkA blockage-sink representation of jet interference effects for noncircular jet orifices19700002529WorkDevelopment of an analytical model for the flow of a jet into a subsonic crosswind19700002530WorkNumerical treatment of line singularities for modelling a jet in a low-speed cross flow19700002531WorkAnalytic description of jet-wake cross sections for a jet normal to a subsonic free stream19700002532WorkCross wind effects on trajectory and cross sections of turbulent jets19700002533WorkA general jet efflux simulation model19700002534WorkCalculation of jet interference effects on V/STOL aircraft by a nonplanar potential flow method19700002535WorkInviscid models for the pressure induced by a jet transverse to a subsonic stream19700002536WorkThe Use of Matched Asymptotic Expansions as an Approach to the Problem of the Jet in A Cross Flow19700002537WorkMass entrainment of a circular jet in a cross flow
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