Shock tube investigation of dynamic response of pressure transducers for validation of rotor performance measurements
By: submitted by Daniel Bershader.
Contributors: United States. National Aeronautics and Space Administration.
Series: NASA-CR -- 182673.; NASA contractor report -- NASA CR-182673.
Publisher: Department of Aeronautics and Astronautics, Stanford University
Published: 1989
Place of publication: Stanford, Calif
Language: eng
Format: Microform
Subjects: Shock tubes.; Transducers.; Rotors.
Notes: Distributed to depository libraries in microfiche.

Microfiche. [Washington, D.C.? : National Aeronautics and Space Administration], 1989. 1 microfiche.