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The design of test-section inserts for higher speed aeroacoustic testing in the Ames 80- by 120-foot wind tunnel

The design of test-section inserts for higher speed aeroacoustic testing in the Ames 80- by 120-foot wind tunnel

By Paul T. Soderman

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Publish Date

1992

Publisher

National Aeronautics and Space Administration, Ames Research Center,For sale by the National Technical Information Service

Language

eng

Pages

-

1-4 of 4 Editions

The design of test-section inserts for higher speed aeroacoustic testing in the Ames 80- by 120-foot wind tunnel

View The design of test-section inserts for higher speed aeroacoustic testing in the Ames 80- by 120-foot wind tunnel
The design of test-section inserts for higher speed aeroacoustic testing in the Ames 80- by 120-foot wind tunnel

Language: eng

Published In: 1992

Publisher: National Aeronautics and Space Administration, Ames Research Center, For sale by the National Technical Information Service

The design of test-section inserts for higher speed aeroacoustic testing in the Ames 80- by 120-foot wind tunnel

View The design of test-section inserts for higher speed aeroacoustic testing in the Ames 80- by 120-foot wind tunnel
The design of test-section inserts for higher speed aeroacoustic testing in the Ames 80- by 120-foot wind tunnel

Language: eng

Published In: 1992

Publisher: National Aeronautics and Space Administration, Ames Research Center, For sale by the National Technical Information Service

The design of test-section inserts for higher speed aeroacoustic testing in the Ames 80- by 120-foot wind tunnel

View The design of test-section inserts for higher speed aeroacoustic testing in the Ames 80- by 120-foot wind tunnel
The design of test-section inserts for higher speed aeroacoustic testing in the Ames 80- by 120-foot wind tunnel

Language: eng

Published In: 1992

Publisher: National Aeronautics and Space Administration, Ames Research Center, For sale by the National Technical Information Service

The design of test-section inserts for higher speed aeroacoustic testing in the Ames 80- by 120-foot wind tunnel

View The design of test-section inserts for higher speed aeroacoustic testing in the Ames 80- by 120-foot wind tunnel
The design of test-section inserts for higher speed aeroacoustic testing in the Ames 80- by 120-foot wind tunnel

Language: eng

Published In: 1992

Publisher: National Aeronautics and Space Administration, Ames Research Center, For sale by the National Technical Information Service