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ElectronicResource GovDoc
Author
Gangwani, Santu T.
Title
Synthesized airfoil data method for prediction of dynamic stall and unsteady airloads [electronic resource] / Santu T. Gangwani.
Imprint
[Washington D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1983.
Connect to
Connect to https://permanent.fdlp.gov/lps104922/LPS104922/ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19850009696_1985009696.pdf
Copies
Location
Call No.
OPAC Message
Status
Axe Federal Documents Online
NAS 1.26:3672
---
Available
Description
1 v.
Series
NASA contractor report ; 3672
NASA contractor report ; NASA CR-3672.
Form
Mode of access via the NTRS web site.
Reproduction
Microfiche. [Washington, D.C. : National Aeronautics and Space Administration], 1985. 2 microfiches.
Subject
Aerodynamic stalling.
Airfoils.
Prediction analysis techniques.
Rotor aerodynamics.
Added Author
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Gpo Item No.
0830-H-14 (online)
Sudoc No.
NAS 1.26:3672
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