Investigation of a Three-blade Propeller in Combination with Two Different Spinners and an NACA D-type Cowl at Mach Numbers Up to 0.80

Investigation of a Three-blade Propeller in Combination with Two Different Spinners and an NACA D-type Cowl at Mach Numbers Up to 0.80
Title Investigation of a Three-blade Propeller in Combination with Two Different Spinners and an NACA D-type Cowl at Mach Numbers Up to 0.80 PDF eBook
Author George C. Kenyon
Publisher
Pages 68
Release 1954
Genre Aerodynamics
ISBN

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EFFECTS OF TWO SPINNER SHAPES ON THE PRESSURE RECOVERY IN AN NACA 1-SERIES D-TYPE COWL BEHIND A THREE-BLADE PROPELLER AT MACH NUMBERS UP TO 0.80

EFFECTS OF TWO SPINNER SHAPES ON THE PRESSURE RECOVERY IN AN NACA 1-SERIES D-TYPE COWL BEHIND A THREE-BLADE PROPELLER AT MACH NUMBERS UP TO 0.80
Title EFFECTS OF TWO SPINNER SHAPES ON THE PRESSURE RECOVERY IN AN NACA 1-SERIES D-TYPE COWL BEHIND A THREE-BLADE PROPELLER AT MACH NUMBERS UP TO 0.80 PDF eBook
Author
Publisher
Pages 38
Release 1954
Genre
ISBN

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Subject Index to Unclassified ASTIA Documents

Subject Index to Unclassified ASTIA Documents
Title Subject Index to Unclassified ASTIA Documents PDF eBook
Author Defense Documentation Center (U.S.)
Publisher
Pages 906
Release 1960
Genre Industrial arts
ISBN

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Advanced Turboprop Project

Advanced Turboprop Project
Title Advanced Turboprop Project PDF eBook
Author Roy D. Hager
Publisher
Pages 140
Release 1988
Genre Airplanes
ISBN

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Sensing surface PEGylation with microcantilevers

Sensing surface PEGylation with microcantilevers
Title Sensing surface PEGylation with microcantilevers PDF eBook
Author
Publisher
Pages
Release 2010
Genre
ISBN

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Investigation of the NACA-4-(3)(08)-03 Two-blade Propeller at Forward Mach Numbers to 0.925

Investigation of the NACA-4-(3)(08)-03 Two-blade Propeller at Forward Mach Numbers to 0.925
Title Investigation of the NACA-4-(3)(08)-03 Two-blade Propeller at Forward Mach Numbers to 0.925 PDF eBook
Author James B. Delano
Publisher
Pages 34
Release 1949
Genre Charts, diagrams, etc
ISBN

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An investigation of the NACA-4-(3)(08)-03 two-blade propeller has been made in the Langley 8-foot high-speed tunnel for blade angles of 55, 60, and 65 degrees at Mach numbers up to 0.925. Comparison of the force-test measurements obtained for the NACA-4-(3)(08)-03 two-blade propeller with those previously obtained for the NACA-4-(5)(08)-03 two-blade propeller indicates that the differences in design lift coefficient were insufficient to produce appreciable changes in maximum efficiency over the range of blade angle and Mach number investigated.

Investigation of the NACA 4-(0)(03)-45 Two-blade Propeller at Forward Mach Numbers to 0.925

Investigation of the NACA 4-(0)(03)-45 Two-blade Propeller at Forward Mach Numbers to 0.925
Title Investigation of the NACA 4-(0)(03)-45 Two-blade Propeller at Forward Mach Numbers to 0.925 PDF eBook
Author Melvin M. Carmel
Publisher
Pages 34
Release 1950
Genre Mach number
ISBN

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