Airfoil Modification Effects on Subsonic and Transonic Pressure Distributions and Performance for the EA-6B Airplane

Airfoil Modification Effects on Subsonic and Transonic Pressure Distributions and Performance for the EA-6B Airplane

Author(s):

Publication title:

NASA Technical Reports

Pub. Year:

1995

Issue:

NASA-CR-3516

No.:

H1/02 0049059

Pt.:

NAS 1.26:3516

Paper no.:

N95-26382

Page(from):

1

Page(to):

86

Pages:

86

Pub. info.:

National Aeronautics and Space Adminstration

Language:

English

Type:

Technical Paper

Details

TDL ID:

ZA00001431

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