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ElectronicResource GovDoc
Author Ramakrishnan, Sekaripuram.

Title Supersonic flow computations for an ASTOVL aircraft configuration [electronic resource] : phase 2, part 2 / Sekaripuram Ramakrishnan, Sukumar R. Chakravarthy, and Kuo-Yen Szema.

Imprint [Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1990.

Copies

Location Call No. OPAC Message Status
 Axe Federal Documents Online  NAS 1.26:4284    ---  Available
Description 1 v.
Series NASA contractor report ; 4284
NASA contractor report ; NASA CR-4284.
Note "Prepared for Langley Research Center under contract NAS1-17492."
Form Mode of access via the NTRS web site.
Bibliography Includes bibliographical references.
Subject Aircraft configurations.
Computational fluid dynamics.
Design analysis.
Grid generation (Mathematics)
Supersonic flow.
V/STOL aircraft.
Added Author Chakravarthy, Sukumar R.
Szema, Kuo-Yen.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Langley Research Center.
Gpo Item No. 0830-H-14 (online)
Sudoc No. NAS 1.26:4284

 
    
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