Design and Performance of a High-pressure-ratio, Highly Loaded Axial-flow Transonic Compressor Space Author: George W. Lewis (Jr.) Publisher: Published: 1974 Total Pages: 100 ISBN-13: DOWNLOAD EBOOK →
Design and Performance of a High-pressure-ratio, Highly Loaded Axial-flow Transonic Compressor Stage Author: George W. Lewis (Jr.) Publisher: Published: 1974 Total Pages: 0 ISBN-13: DOWNLOAD EBOOK →
Design and Performance of a High-pressure-ratio, Highly Loaded Axial-flow Transonic Compressor Space Author: G. W. Lewis (Jr) Publisher: Published: 1974 Total Pages: ISBN-13: DOWNLOAD EBOOK →
Performance of Single-stage Axial-flow Transonic Compressor with Rotor and Stator Aspect Ratios of 1.19 and 1.26 Respectively, and with Design Pressure Ratio of 2.05 Author: Royce D. Moore Publisher: Published: 1980 Total Pages: 108 ISBN-13: DOWNLOAD EBOOK →
Design and Performance of a High-pressure-ratio, Highly Loaded Axial-flow Transonic Compressor Space Author: George W. Lewis (Jr.) Publisher: Published: 1974 Total Pages: 100 ISBN-13: DOWNLOAD EBOOK →
Performance of Single-stage Axial-flow Transonic Compressor with Rotor and Stator Aspect Ratios of 1.19 and 1.26, Respectively, and with Design Pressure Ration of 1.82 Author: Lonnie Reid Publisher: Published: 1978 Total Pages: 110 ISBN-13: DOWNLOAD EBOOK →
Performance of Single-stage Axial-flow Transonic Compressor with Rotor and Stator Aspect Ratios of 1.63 and 1.77, Respectively, and with Design Pressure Ratio of 2.05 Author: Royce D. Moore Publisher: Published: 1982 Total Pages: 120 ISBN-13: DOWNLOAD EBOOK →
Performance of Single-stage Axial-flow Transonic Compressor with Rotor and Stator Aspect Ratios of 1.63 and 1.78, Respectively, and with Design Pressure Ratio of 1.82 Author: Royce D. Moore Publisher: Published: 1982 Total Pages: 120 ISBN-13: DOWNLOAD EBOOK →
Performance of Single-stage Axial-flow Transonic Compressor with Rotor and Stator Aspect Ratios of 1.63 and 1.77, Respectively, and with Design Pressure Ratio of 2.05 Author: Royce D. Moore Publisher: Published: 1982 Total Pages: 120 ISBN-13: DOWNLOAD EBOOK →
Performance of Single-stage Axial-flow Transonic Compressor with Rotor and Stator Aspect Ratios of 1.19 and 1.26, Respectively, and with Design Pressure Ratio of 2.05 Author: Royce D. Moore Publisher: Published: 1978 Total Pages: ISBN-13: DOWNLOAD EBOOK →