Hot Gas Ingestion Test Results of a Two-Poster Vectored Thrust Concept with Flow Visualization in the NASA Lewis 9-by 15-Foot Low Speed Wind Tunnel

Hot Gas Ingestion Test Results of a Two-Poster Vectored Thrust Concept with Flow Visualization in the NASA Lewis 9-by 15-Foot Low Speed Wind Tunnel

Author(s):

Johns, Albert L. ( National Aeronautics and Space Adminisration Lewis Research Center )

Publication title:

NASA Technical Reports

Pub. Year:

1990

Issue:

NASA-TM-103258

Pt.:

NAS 1.15:103258

Paper no.:

N91-21116

Page(from):

1

Page(to):

27

Pages:

27

Pub. info.:

National Aeronautics and Space Adminstration

Language:

English

Type:

Technical Paper

Details

TDL ID:

ZA00001427

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