| Author | : Edward J. Marquart |
| File Size | : 44,6 Mb |
| Publisher | : Unknown |
| Language | : English |
| Release Date | : 24 April 1982 |
| ISBN | : UOM:39015104952166 |
| Pages | : 44 pages |
Download or read online Sting Interference Effects on the Modified Basic Finner Missile at Mach Numbers 0 3 Through 1 3 written by Edward J. Marquart, published by Unknown which was released on 1982. Get Sting Interference Effects on the Modified Basic Finner Missile at Mach Numbers 0 3 Through 1 3 Books now! Available in PDF, ePub and
Get BookDownload or read online Technical Abstract Bulletin written by Anonim, published by Unknown which was released on 1982. Get Technical Abstract Bulletin Books now! Available in PDF, ePub and Kindle.
Get BookWind tunnel tests were conducted to provide support interference information for planning and directing wind tunnel tests at supersonic and hypersonic Mach numbers. Sting-length and sting-diameter effects on base and surface pressures of a blunt 6-deg cone with a sliced base were investigated at Mach numbers 2, 3, 5, and 8. Dynamic stability tests
Get BookWind tunnel tests were conducted to provide sting-support interference information for planning and directing wind tunnel tests at subsonic and transonic Mach numbers. Sting-length effects on dynamic stability derivatives, static pitching moment, and base pressure of a blunt, flat-base 7- deg cone were investigated at Mach numbers 0.2 to 1.3 in the
Get BookWind tunnel sting support interference effects on dynamic stability derivatives, static pitching moment and base pressure of a blunt, 7-deg cone were investigated at subsonic and transonic Mach numbers. The cone was tested with sting configurations having a variable effective sting length ranging from 1 to 3.3 model base diameters, at angles
Get Book
Wind tunnel sting support interference effects on dynamic stability derivatives, static pitching moment and base pressure of a blunt, 7-deg cone were investigated at subsonic and transonic Mach numbers. The cone was tested with sting configurations having a variable effective sting length ranging from 1 to 3.3 model base diameters, at angles
Get BookMeasurements were made to determine the effects of sting-support diameter on the base pressures of an elliptic cone with ratio of cross-section thickness to width of 1/3 and a plan-form, semi-apex angle of 15 deg. The investigation was made for model angles of attack from -2 deg to +20 deg at Mach numbers
Get Book
Wind tunnel sting support interference effects on dynamic stability derivatives, static pitching moment and base pressure of a blunt, 7-deg cone were investigated at subsonic and transonic Mach numbers. The cone was tested with sting configurations having a variable effective sting length ranging from 1 to 3.3 model base diameters, at angles
Get Book