Large-scale aeroacoustic research feasibility and conceptual design of test-section inserts for the Ames 80- by 120-foot wind tunnel

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National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1990 - Technology & Engineering - 45 pages
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Contents

40 by 80FOOT OPEN JET FOR 150 knots AIRSPEED
9
APPENDIX A PRESSURE LOSS EQUATIONS
17
TABLES
23

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