Download or read book 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 written by George C. Kenyon and published by . This book was released on 1954 with total page 68 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book 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 written by and published by . This book was released on 1954 with total page 38 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Sensing surface PEGylation with microcantilevers written by and published by . This book was released on 2010 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Investigation of the NACA 4 0 03 45 Two blade Propeller at Forward Mach Numbers to 0 925 written by Melvin M. Carmel and published by . This book was released on 1950 with total page 34 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Investigation of the NACA 4 3 08 03 Two blade Propeller at Forward Mach Numbers to 0 925 written by James B. Delano and published by . This book was released on 1949 with total page 34 pages. Available in PDF, EPUB and Kindle. Book excerpt: 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.
Download or read book Investigation of the NACA 4 4 06 04 Two blade Propeller at Forward Mach Numbers to 0 925 written by James B. Delano and published by . This book was released on 1949 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt: Investigations of the NACA-4-(4)(06)-04 two-blade propeller (design thickness, 0.06 at 0.7-radius station) have been made in the Langley 8-foot high-speed wind tunnel for blade angles from 20 to 70 degrees for forward Mach number up to 0.925.
Download or read book An Investigation of a Four blade Single rotation Propeller in Combination with an Naca 1 series D type Cowling at Mach Numbers Up to 0 83 written by and published by . This book was released on 1953 with total page 74 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Investigation of an NACA 4 5 05 041 Four blade Propeller with Several Spinners at Mach Numbers Up to 0 90 written by Robert M. Reynolds and published by . This book was released on 1952 with total page 86 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Investigation at Mach Numbers to 1 04 of Blade loading Characteristics of Two Full scale Three blade Supersonic Propellers Differing in Blade section Camber written by Leland B. Jr Salters and published by . This book was released on 1957 with total page 46 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Investigation of the NACA 4 5 08 03 Two blade Propeller at Forward Mach Numbers to 0 925 written by James B. Delano and published by . This book was released on 1949 with total page 61 pages. Available in PDF, EPUB and Kindle. Book excerpt: Investigations of the NACA4-(5) (08)-03 two-blade propeller have been made in the Langley 8-foot high-speed tunnel for blade angles from 20 to 70 degrees for forward Mach numbers up to 0.925.
Download or read book Investigation of NACA 4 0 03 045 and NACA 4 0 08 045 Two blade Propellers at Forward Mach Numbers to 0 925 written by James B. Delano and published by . This book was released on 1950 with total page 22 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Investigation of the NACA 3 3 05 05 Eight blade Dual rotating Propeller at Forward Mach Numbers to 0 925 written by Robert J. Platt and published by . This book was released on 1950 with total page 42 pages. Available in PDF, EPUB and Kindle. Book excerpt: Force tests were made on an NACA 3-(3)(05)-05 eight-blade dual-rotating propeller in the Langley 8-foot high-speed tunnel. The tests covered a blade-angle range from 55 to 80 degrees at forward Mach numbers to 0.925.
Download or read book Flight Investigation in Climb and at High Speed Or a Two blade and Three blade Propeller written by Jerome B. Hammack and published by . This book was released on 1949 with total page 672 pages. Available in PDF, EPUB and Kindle. Book excerpt: This report contains the results obtained with a propeller in a three-blade and two-blade configuration in climb and high-speed flight when mounted on a slender-nose fighter airplane. An extensive series of power loadings were investigated up to an airplane Mach number of 0.7. The results are explained by theory. Recommendations for propeller efficiency improvement are stated.
Download or read book Advanced Turboprop Project written by Roy D. Hager and published by . This book was released on 1988 with total page 140 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book An investigation of single and dual rotation propellers at positive and negative thrust and in combinationa with an NACA 1 series d type cowling at Mach numbers up to 0 84 written by Robert M. Reynolds and published by . This book was released on 1957 with total page 58 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Investigation of the NACA 1 167 0 03 058 and NACA 1 167 0 05 058 Three blade Propellers at Forward Mach Numbers to 0 92 Including Effects of Thrust axis Inclination written by Fred A. Demele and published by . This book was released on 1953 with total page 61 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Investigation of the Normal Force Accompanying Thrust axis Inclination of the NACA 1 167 0 03 058 and the NACA 1 167 0 05 058 Three blade Propellers at Forward Mach Numbers to 0 90 written by Fred A. Demele and published by . This book was released on 1954 with total page 31 pages. Available in PDF, EPUB and Kindle. Book excerpt:
