Download or read book On the Free Flight Drag Determination of a Finned Configuration RM 10 Flying at Critical Reynolds Numbers written by John D. Nicolaides and published by . This book was released on 1953 with total page 42 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Subject Index to Unclassified ASTIA Documents written by Defense Documentation Center (U.S.) and published by . This book was released on 1960 with total page 308 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Flight Measurements of Drag and Base Pressure of a Fin stabilized Parabolic Body of Revolution NACA RM 10 at Different Reynolds Numbers and at Mach Numbers from 0 9 to 3 3 written by H. Herbert Jackson and published by . This book was released on 1950 with total page 21 pages. Available in PDF, EPUB and Kindle. Book excerpt: Free-flight tests have been made to investigate the total drag and base drag at different Reynolds numbers of full-scale and half-scale models of an NACA research model designated the RM-10. The general shape of the body was a parabola of revolution of fineness ratio 12.2 with a blunt nose to provide space for the rocket jet. The models were stabilized by four 60 degree sweptback fins mounted at the base of the bodies.

Download or read book A Review of Measurements on AGARD Calibration Models written by North Atlantic Treaty Organization. Advisory Group for Aeronautical Research and Development and published by . This book was released on 1961 with total page 272 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Aero space Engineering written by and published by . This book was released on 1958 with total page 1508 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Aeronautical Engineering Review written by and published by . This book was released on 1957 with total page 844 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Large scale Flight Measurements of Zero lift Drag and Low lift Drag of 10 Wing body Configurations at Mach Numbers from 0 8 to 1 6 written by John D. Morrow and published by . This book was released on 1953 with total page 58 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Aeronautical Engineering Index written by and published by . This book was released on 1954 with total page 1212 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Aerospace Engineering Index written by and published by . This book was released on 1960 with total page 292 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Free flight Measurements of the Transonic Drag Characteristics of Low fineness ratio Cylinders Including Stabilizing Plates and Flares and Varying Nose Bluntness written by Joseph H. Judd and published by . This book was released on 1960 with total page 20 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Average Skin friction Drag Coefficients from Tank Tests of a Parabolic Body of Revolution NACA RM 10 written by Elmo J. Mottard and published by . This book was released on 1953 with total page 26 pages. Available in PDF, EPUB and Kindle. Book excerpt: Average skin-friction drag coefficients were obtained from boundary-layer total-pressure measurements on a parabolic body of revolution (NACA RM-10) basic fineness ratio 15 in water at Reynolds numbers from 4,400,000 to 70,000,000. The tests were made in the Langley tank no. 1 with the body sting-mounted at a depth of two maximum body diameters. The arithmetic mean of three drag measurements taken around the body was in good agreement with flat-palte results, but, apparently because of the slight surface wave casue by the body, the distribution of the boundary layer around the body was not uniform over part of the Reynolds number range.

Download or read book Free flight Range Measurements of Sphere Drag at Low Reynolds Numbers and Low Mach Numbers written by W. R. Lawrence and published by . This book was released on 1967 with total page 19 pages. Available in PDF, EPUB and Kindle. Book excerpt: The drag coefficients of spheres were obtained from free-flight range tests of metal spheres at Reynolds numbers from 185 to 11,600 and at Mach numbers from 0.17 to 0.99. An analysis of the data indicates that the total errors in the measured drag coefficients are within +2 or -2 percent. (Author).

Download or read book Free flight Range Measurements of Sphere Drag at Low Reynolds Numbers and Low Mach Numbers written by and published by . This book was released on 1967 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt: The drag coefficients of spheres were obtained from free-flight range tests of metal spheres at Reynolds numbers from 185 to 11,600 and at Mach numbers from 0.17 to 0.99. An analysis of the data indicates that the total errors in the measured drag coefficients are within +2 or -2 percent. (Author).

Download or read book Drag N Fly written by National Aeronautics and Space Administration (NASA) and published by Createspace Independent Publishing Platform. This book was released on 2018-07-17 with total page 124 pages. Available in PDF, EPUB and Kindle. Book excerpt: The Drag-n-Fly is a remotely piloted, low Reynolds number vehicle. It was designed to maintain level controlled flight and fly a closed course at flight speeds corresponding to Reynolds numbers of less than 2 x 10(exp 5) and as close to 1 x 10(exp 5) as possible. The success of the mission will be associated with achieving the lowest mean chord Reynolds number possible and maximizing loiter time on the course. The flight plan for the Drag-n-Fly calls for the vehicle to ascent to a cruise altitude of 25 ft. The airfoil selected for the Drag-n-Fly is a Spica chosen for its high lift coefficient at low Reynolds number. The propulsion system for the Drag-n-Fly consists of a 10 inch diameter propeller mounted on the front of the vehicle. Structural support for the Drag-n-Fly comes from four box beams running the length of the fuselage. The tail and horizontal stabilizers are located far aft of the lifting surface in order to assure proper static stability. The present design for the Drag-n-Fly will meet the criteria for the present mission. Foohey, Mark and Niehaus, John and Neumann, Jenny and Deviny, Pat and Zurovchak, Jerry and Brenner, Joey and Gendron, Peter Unspecified Center AERODYNAMIC COEFFICIENTS; AIRFOILS; FLIGHT CONTROL; FUSELAGES; LOW REYNOLDS NUMBER; STABILIZERS (FLUID DYNAMICS); STATIC STABILITY; STATIONKEEPING; ASCENT; BOX BEAMS; FLIGHT PLANS; LIFT; PROPELLERS...

Download or read book Drag N Fly written by National Aeronautics and Space Adm Nasa and published by . This book was released on 2018-11-13 with total page 124 pages. Available in PDF, EPUB and Kindle. Book excerpt: The Drag-n-Fly is a remotely piloted, low Reynolds number vehicle. It was designed to maintain level controlled flight and fly a closed course at flight speeds corresponding to Reynolds numbers of less than 2 x 10(exp 5) and as close to 1 x 10(exp 5) as possible. The success of the mission will be associated with achieving the lowest mean chord Reynolds number possible and maximizing loiter time on the course. The flight plan for the Drag-n-Fly calls for the vehicle to ascent to a cruise altitude of 25 ft. The airfoil selected for the Drag-n-Fly is a Spica chosen for its high lift coefficient at low Reynolds number. The propulsion system for the Drag-n-Fly consists of a 10 inch diameter propeller mounted on the front of the vehicle. Structural support for the Drag-n-Fly comes from four box beams running the length of the fuselage. The tail and horizontal stabilizers are located far aft of the lifting surface in order to assure proper static stability. The present design for the Drag-n-Fly will meet the criteria for the present mission. Foohey, Mark and Niehaus, John and Neumann, Jenny and Deviny, Pat and Zurovchak, Jerry and Brenner, Joey and Gendron, Peter Unspecified Center AERODYNAMIC COEFFICIENTS; AIRFOILS; FLIGHT CONTROL; FUSELAGES; LOW REYNOLDS NUMBER; STABILIZERS (FLUID DYNAMICS); STATIC STABILITY; STATIONKEEPING; ASCENT; BOX BEAMS; FLIGHT PLANS; LIFT; PROPELLERS...

Download or read book An Analysis of Flight Test Data on the C 141A Aircraft written by and published by . This book was released on 1970 with total page 180 pages. Available in PDF, EPUB and Kindle. Book excerpt: This study comprises part of a research program to investigate the degree of correlation attainable between flight test measured airplane drag levels and the full scale drag that would be predicted on the basis of wind tunnel data.

Download or read book Preliminary Full scale Power off Drag of the X 15 Airplane for Mach Numbers from 0 7 to 3 1 written by Edwin J. Saltzman and published by . This book was released on 1960 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt: