Roll-yaw control at high angle of attack by forebody tangential blowing

Roll-yaw control at high angle of attack by forebody tangential blowing

Author(s):

Pedreiro, N. ( Stanford Univ. )
Rock, S. M. ( Stanford Univ. )
Celik, Z. Z. ( Stanford Univ. )
Roberts, L. ( Stanford Univ. )

Publication title:

NASA Technical Reports

Pub. Year:

1995

Vol.:

19960038364

Issue:

NASA-CR-201481

Pt.:

NAS 1.26:201481

Paper no.:

N96-30838

Page(from):

1

Page(to):

28

Pages:

28

Pub. info.:

National Aeronautics and Space Adminstration

Language:

English

Type:

Technical Paper

Details

TDL ID:

ZA00001432

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