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Book Investigation of the NACA 4  3  08  03 Two blade Propeller at Forward Mach Numbers to 0 925

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.

Book Investigation of the NACA 4  4  06  04 Two blade Propeller at Forward Mach Numbers to 0 925

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.

Book Investigation of the NACA 4  5  08  03 Two blade Propeller at Forward Mach Numbers to 0 925

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.

Book Investigation of the NACA 4  3  08  03 and NACA 4  3  08  045 Two blade Propellers at Forward Mach Numbers to 0 725 to Determine the Effects of Compressibillity and Solidity on Performance

Download or read book Investigation of the NACA 4 3 08 03 and NACA 4 3 08 045 Two blade Propellers at Forward Mach Numbers to 0 725 to Determine the Effects of Compressibillity and Solidity on Performance written by John Stack and published by . This book was released on 1950 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Investigation of the NACA 4  3  08  03 and NACA 4  3  08  045 Two blade Propellers at Forward Mach Numbers to 0 725 to Determine the Effects of Compressibility and Solidity on Performance

Download or read book Investigation of the NACA 4 3 08 03 and NACA 4 3 08 045 Two blade Propellers at Forward Mach Numbers to 0 725 to Determine the Effects of Compressibility and Solidity on Performance written by John Stack and published by . This book was released on 1950 with total page 32 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Investigation of the NACA 4  5  08  03 and NACA 4  10  08  03 Two blade Propellers at Forward Mach Numbers to 0  725 to Determine the Effects of Camber and Compressibility on Performance

Download or read book Investigation of the NACA 4 5 08 03 and NACA 4 10 08 03 Two blade Propellers at Forward Mach Numbers to 0 725 to Determine the Effects of Camber and Compressibility on Performance written by James B. Delano and published by . This book was released on 1951 with total page 31 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Further Investigation of NACA 4  5  08  03 Two blade Propeller at High Forward Speeds

Download or read book Further Investigation of NACA 4 5 08 03 Two blade Propeller at High Forward Speeds written by Melvin M. Carmel and published by . This book was released on 1947 with total page 50 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Investigation of the NACA 3  3  05  05 Eight blade Dual rotating Propeller at Forward Mach Numbers to 0 925

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.

Book Investigation of the NACA 4  4  06  057 45A and NACA 4  4  06  57 45B Two blade Swept Propellers at Forward Mach Numbers to 0 925

Download or read book Investigation of the NACA 4 4 06 057 45A and NACA 4 4 06 57 45B Two blade Swept 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 44 pages. Available in PDF, EPUB and Kindle. Book excerpt: Investigations of the NACA 4-(14)(06)-057-45A and NACA 4-(4)(06)-057-45B two-blade swept propellers have been made in the Langley 8-foot high-speed tunnel at blade angles of 25, 55, 60, 65, and 70 degrees. The maximum forward Mach number reached in these investigations was 0.925.

Book Effect of Compressibility and Camber as Determined from an Investigation of the NACA 4  3  08  03 and 4  5  08  03 Two blade Propellers Up to Forward Mach Numbers of 0 925

Download or read book Effect of Compressibility and Camber as Determined from an Investigation of the NACA 4 3 08 03 and 4 5 08 03 Two blade Propellers Up to Forward Mach Numbers of 0 925 written by Melvin M. Carmel and published by . This book was released on 1950 with total page 92 pages. Available in PDF, EPUB and Kindle. Book excerpt: Tests of the NACA 4-(3)(08)-03 and 4-(5)(08)-03 two-blade propellers were conducted in the Langley 8-foot high-speed tunnel for blade angles between 40 and 65 degrees and through a Mach number range up to 0.925.

Book Investigation of the NACA 4  5  05  037 Six  and Eight blade Dual Rotation Propellers at Positive and Negative Thrust at Mach Numbers Up to 0 90  Including Some Aerodynamic Characteristics of the NACA 4  5  05  041 Two and Four blade  Single rotation Propellers

Download or read book Investigation of the NACA 4 5 05 037 Six and Eight blade Dual Rotation Propellers at Positive and Negative Thrust at Mach Numbers Up to 0 90 Including Some Aerodynamic Characteristics of the NACA 4 5 05 041 Two and Four blade Single rotation Propellers written by John H. Walker and published by . This book was released on 1954 with total page 148 pages. Available in PDF, EPUB and Kindle. Book excerpt: