Assessment of Dual-Point Drag Reduction for an Executive-Jet Modified Airfoil Section

Assessment of Dual-Point Drag Reduction for an Executive-Jet Modified Airfoil Section

Author(s):

Publication title:

NASA Technical Reports

Pub. Year:

1996

Vol.:

19960039925

Issue:

NASA-TP-3579

Pt.:

NAS 1.60:3579

Paper no.:

N96-31079

Page(from):

1

Page(to):

126

Pages:

126

Pub. info.:

National Aeronautics and Space Adminstration

Language:

English

Type:

Technical Paper

Details

TDL ID:

ZA00001432

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