Reynolds Number Effects on Leading Edge Radius Variations of a Supersonic Transport at Transonic Conditions

Reynolds Number Effects on Leading Edge Radius Variations of a Supersonic Transport at Transonic Conditions

Author(s):

Rivers,S.M.B. ( NASA Langley Research Center )
Wahls,R.A.
Owens,L.R.

Publication title:

AIAA paper

Title of ser.:

AIAA Paper : AIAA Applied Aerodynamics Conference

Ser. no.:

2001

Pub. Year:

2001

No.:

2001-2462

Paper no.:

AIAA-2001-2462

Page(from):

1

Page(to):

19

Pages:

19

Pub. info.:

Reston, VA: American Institute of Aeronautics and Astronautics

ISSN:

01463705

Language:

English

Call no.:

A07400

Type:

Technical Paper

Details

TDL ID:	ZA00050822
Series ID:	PA00000157
Conf. info. (Name):	AIAA Applied Aerodynamics Conference
Conf. info. (Number):	19th
Conf. info. (Venue):	Anaheim, CA
Conf. info. (Date):	2001.06.11-2001.06.14
Note for article:	19th AIAA Applied Aerodynamics Conference 11-14 June 2001 Anaheim, California

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