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Danielle Koch (44 results)
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Condition: New.
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Crisis Mode (Paperback or Softback)
Language: English
Published by Bookleaf Publishing 8/4/2025, 2025
ISBN 10: 9370926054 ISBN 13: 9789370926059
Paperback or Softback. Condition: New. Crisis Mode. Book.
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Paperback or Softback. Condition: New. Mean Flow and Noise Prediction for a Separate Flow Jet with Chevron Mixers. Book.
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Condition: As New. Unread book in perfect condition.
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Condition: As New. Unread book in perfect condition.
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Crisis Mode
Seller: GreatBookPricesUK, Woodford Green, United Kingdom
Seller rating 5 out of 5 stars
US$ 18.26
US$ 20.16 shipping
Ships from United Kingdom to U.S.A.Quantity: Over 20 available
Add to basketCondition: New.
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Mean Flow and Noise Prediction for a Separate Flow Jet With Chevron Mixers
Seller: GreatBookPricesUK, Woodford Green, United Kingdom
Seller rating 5 out of 5 stars
US$ 18.84
US$ 20.16 shipping
Ships from United Kingdom to U.S.A.Quantity: Over 20 available
Add to basketCondition: As New. Unread book in perfect condition.
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Crisis Mode
Seller: GreatBookPricesUK, Woodford Green, United Kingdom
Seller rating 5 out of 5 stars
US$ 19.59
US$ 20.16 shipping
Ships from United Kingdom to U.S.A.Quantity: Over 20 available
Add to basketCondition: As New. Unread book in perfect condition.
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Mean Flow and Noise Prediction for a Separate Flow Jet With Chevron Mixers
Seller: GreatBookPricesUK, Woodford Green, United Kingdom
Seller rating 5 out of 5 stars
US$ 27.51
US$ 20.16 shipping
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MEDIEVALES 10, Presses du Centre d'Etudes Médiévales, Université de Picardie-Jules Verne, sans date, 146 p., broché, bon état et intérieur très propre. Articles en français et en allemand.
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Design and Performance Calculations of a Propeller for Very High Altitude Flight
Seller: Ria Christie Collections, Uxbridge, United Kingdom
Seller rating 5 out of 5 stars
US$ 63.10
US$ 16.10 shipping
Ships from United Kingdom to U.S.A.Quantity: Over 20 available
Add to basketCondition: New. In.
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BPM. Condition: New. New Book. Shipped from UK. THIS BOOK IS PRINTED ON DEMAND. Established seller since 2000.
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Design and Performance Calculations of a Propeller for Very High Altitude Flight
Seller: GreatBookPricesUK, Woodford Green, United Kingdom
Seller rating 5 out of 5 stars
US$ 62.43
US$ 20.16 shipping
Ships from United Kingdom to U.S.A.Quantity: Over 20 available
Add to basketCondition: New.
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Crisis Mode (Edition1st)
Seller: PBShop.store UK, Fairford, GLOS, United Kingdom
Seller rating 5 out of 5 stars
US$ 18.28
US$ 4.42 shipping
Ships from United Kingdom to U.S.A.Quantity: Over 20 available
Add to basketBPM. Condition: New. New Book. Delivered from our UK warehouse in 4 to 14 business days. THIS BOOK IS PRINTED ON DEMAND. Established seller since 2000.
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Design and Performance Calculations of a Propeller for Very High Altitude Flight
Language: English
Published by Creative Media Partners, LLC, 2025
ISBN 10: 1025158849 ISBN 13: 9781025158846
PAP. Condition: New. New Book. Shipped from UK. THIS BOOK IS PRINTED ON DEMAND. Established seller since 2000.
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Design and Performance Calculations of a Propeller for Very High Altitude Flight
Language: English
Published by Creative Media Partners, LLC Mai 2025, 2025
ISBN 10: 1025158849 ISBN 13: 9781025158846
Taschenbuch. Condition: Neu. Neuware.
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Design and Performance Calculations of a Propeller for Very High Altitude Flight
Language: English
Published by Creative Media Partners, LLC Mai 2025, 2025
ISBN 10: 1025154088 ISBN 13: 9781025154084
Buch. Condition: Neu. Neuware.
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Condition: New. KlappentextrnrnReported here is a design study of a propeller for a vehicle capable of subsonic flight in Earth s stratosphere. All propellers presented were required to absorb 63.4 kW (85 hp) at 25.9 km (85,000 ft) while aircraft cruise velocit.
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Design and Performance Calculations of a Propeller for Very High Altitude Flight
Language: English
Published by Creative Media Partners, LLC, 2025
ISBN 10: 1025158849 ISBN 13: 9781025158846
Seller: PBShop.store UK, Fairford, GLOS, United Kingdom
Seller rating 5 out of 5 stars
US$ 22.01
US$ 4.42 shipping
Ships from United Kingdom to U.S.A.Quantity: Over 20 available
Add to basketPAP. Condition: New. New Book. Delivered from our UK warehouse in 4 to 14 business days. THIS BOOK IS PRINTED ON DEMAND. Established seller since 2000.
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Design and Performance Calculations of a Propeller for Very High Altitude Flight
Language: English
Published by Creative Media Partners, LLC Mär 2013, 2013
ISBN 10: 1288910975 ISBN 13: 9781288910977
Taschenbuch. Condition: Neu. Neuware - Reported here is a design study of a propeller for a vehicle capable of subsonic flight in Earth's stratosphere. All propellers presented were required to absorb 63.4 kW (85 hp) at 25.9 km (85,000 ft) while aircraft cruise velocity was maintained at Mach 0.40. To produce the final design, classic momentum and blade-element theories were combined with two and three-dimensional results from the Advanced Ducted Propfan Analysis Code (ADPAC), a numerical Navier-Stokes analysis code. The Eppler 387 airfoil was used for each of the constant section propeller designs compared. Experimental data from the Langley Low-Turbulence Pressure Tunnel was used in the strip theory design and analysis programs written. The experimental data was also used to validate ADPAC at a Reynolds numbers of 60,000 and a Mach number of 0.20. Experimental and calculated surface pressure coefficients are compared for a range of angles of attack. Since low Reynolds number transonic experimental data was unavailable, ADPAC was used to generate two-dimensional section performance predictions for Reynolds numbers of 60,000 and 100,000 and Mach numbers ranging from 0.45 to 0.75. Surface pressure coefficients are presented for selected angles of attack. in addition to the variation of lift and drag coefficients at each flow condition. A three-dimensional model of the final design was made which ADPAC used to calculated propeller performance. ADPAC performance predictions were compared with strip-theory calculations at design point. Propeller efficiency predicted by ADPAC was within 1.5% of that calculated by strip theory methods, although ADPAC predictions of thrust, power, and torque coefficients were approximately 5% lower than the strip theory results. Simplifying assumptions made in the strip theory account for the differences seen.
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Design and Performance Calculations of a Propeller for Very High Altitude Flight
Seller: GreatBookPricesUK, Woodford Green, United Kingdom
Seller rating 5 out of 5 stars
US$ 166.10
US$ 20.16 shipping
Ships from United Kingdom to U.S.A.Quantity: Over 20 available
Add to basketCondition: As New. Unread book in perfect condition.
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US$ 155.04
US$ 33.60 shipping
Ships from United Kingdom to U.S.A.Quantity: 1 available
Add to basketPaperback. Condition: Like New. LIKE NEW. SHIPS FROM MULTIPLE LOCATIONS. book.
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Condition: As New. Unread book in perfect condition.
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Condition: New. Print on Demand pp. 22.
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Condition: New. Print on Demand pp. 22.
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Condition: New. PRINT ON DEMAND pp. 22.
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Condition: New. Print on Demand.
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Design and Performance Calculations of a Propeller for Very High Altitude Flight
Language: English
Published by Creative Media Partners, LLC, 2025
ISBN 10: 1025154088 ISBN 13: 9781025154084
HRD. Condition: New. New Book. Shipped from UK. THIS BOOK IS PRINTED ON DEMAND. Established seller since 2000.
