Effects of Wing Sweep on In-Flight Boundary-Layer Transition for a Laminar Flow Wing at Mach Numbers From 0.60 to 0.79

Effects of Wing Sweep on In-Flight Boundary-Layer Transition for a Laminar Flow Wing at Mach Numbers From 0.60 to 0.79

Author(s):

Anderson, Bianca Trujillo ( NASA Ames Research Center Dryden Flight Research Facility )
Meyer, Robert R., Jr.

Publication title:

NASA Technical Reports

Pub. Year:

1990

Issue:

NASA-TM-101701

Pt.:

NAS 1.15:101701

Paper no.:

N91-24555

Page(from):

1

Page(to):

37

Pages:

37

Pub. info.:

National Aeronautics and Space Adminstration

Language:

English

Type:

Technical Paper

Details

TDL ID:

ZA00001427

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