NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Collections About News Help Login

Press Enter or click the Search button to begin your search.

Back to Results
Supersonic flow computations for an ASTOVL aircraft configurationA multi-zonal, unified, space/time marching method has been used to solve the Euler and Reynolds-averaged Navier-Stokes equations for supersonic flow past an Advanced Short Take-Off and Vertical Landing (ASTOVL) aircraft configuration. Lift, drag and pitching moment values obtained from the computations compare well with wind-tunnel measurements. The calculations demonstrate the capability of the method used to accurately predict design parameters such as lift, drag and pitching moment for very complex aircraft configurations.
Document ID
19900058792
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Ramakrishnan, S. V.
Szema, K. Y.
Chakravarthy, S. R.
Bihari, B. L.
Date Acquired
August 14, 2013
Publication Date
January 1, 1990
Subject Category
Aerodynamics
Report/Patent Number
AIAA PAPER 90-2997
Report Number: AIAA PAPER 90-2997
Meeting Information
Meeting: AIAA Applied Aerodynamics Conference
Location: Portland, OR
Country: United States
Start Date: August 20, 1990
End Date: August 22, 1990
Accession Number
90A45847
Funding Number(s)
CONTRACT_GRANT: NAS1-17492
Distribution Limits
Public
Copyright
Other

Available Downloads

There are no available downloads for this record.

Related Records

There are no records associated with this record.
No Preview Available