Download or read book Effect of Multiple Jets Exits on the Base Pressure of a Simple Wing Body Combination at Mach Numbers of 0 6 to 1 27 written by and published by . This book was released on 1959 with total page 42 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Effect of Multiple jet Exits on Base Pressure of Simple Wing body Combination at Mach Numbers of 0 6 to 1 27 with List of References written by and published by . This book was released on 1959 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Index to NASA Technical Publications written by United States. National Aeronautics and Space Administration and published by . This book was released on 1960-07 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book U S Government Research Reports written by and published by . This book was released on 1961 with total page 184 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book An Investigation at Mach Numbers 1 94 and 2 41 of Jet Effects Upon the Longitudinal and Directional Stability of a General Aircraft Configuration Employing Wing tip mounted Nacelles written by Frank L. Clark and published by . This book was released on 1958 with total page 74 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Effects of Jet Billowing on Stability of Missile type Bodies at Mach 3 85 written by Reino J. Salmi and published by . This book was released on 1960 with total page 22 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Effects of a Lower Surface Jet on the Lift drag Ratio of a 45 Sweptback Wing at a Mach Number of 2 01 written by Emma Jean Landrum and published by . This book was released on 1960 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Experimental Pressure Distributions Over Two Wing body Combinations at Mach Number 1 9 written by Barry Moskowitz and published by . This book was released on 1951 with total page 40 pages. Available in PDF, EPUB and Kindle. Book excerpt: Abstract: Pressure distributions on two wing-body combinations were obtained at Mach number of 1.9 to investigate wing-body interference. A rectangular wing, a triangular wing, and a cylindrical body having an ogive nose were investigated alone and in combination. Pressure distributions over the wing body combination compared favorable with theoretical calculations based primarily on a generalization of the method of Nielsen and Matteson, except at the root section of wings where boundary layer of body modified the flow.

Download or read book The Flow Past a Straight and a Swept wing body Combination and Their Equivalent Bodies of Revolution at Mach Numbers Near 1 0 written by W. F. Lindsey and published by . This book was released on 1954 with total page 24 pages. Available in PDF, EPUB and Kindle. Book excerpt: Abstract: The complete flow fields past a straight and a swept wing-body combination and their equivalent bodies of revolution at Mach numbers around 1.0 have been observed by means of motion-picture schlieren photography. The results of these observations indicate that the shock growth and positions on the wing-body combinations are closely reproduced in the flow past their respective equivalent bodies.

Download or read book Jet Effects on Base Pressures of Conical Afterbodies at Mach 1 91 and 3 12 written by L. Eugene Baughman and published by . This book was released on 1957 with total page 111 pages. Available in PDF, EPUB and Kindle. Book excerpt: Data are presented which show the effect of a jet on base pressure for a series of conical afterbody-jet-nozzle combinations having boattail angles that varied from o to 11 degrees and base-to-jet diameter ratios that varied from 1.11 to 2.67. The jet nozzles had exit angles from 0 to 20 degrees and were designed for exit Mach numbers from 1.0 to 3.2. Pressure ratios up to 30 tested for both a cold (air) and a hot (rocket) jet. The investigation was conducted at free-stream Mach numbers of 1.91 to 3.12.

Download or read book International Aerospace Abstracts written by and published by . This book was released on 1998 with total page 988 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Exploratory Investigation at Mach Numbers from 0 40 to 0 95 of the Effects of Jets Blown Over a Wing written by Lawrence Elwood Putnam and published by . This book was released on 1973 with total page 76 pages. Available in PDF, EPUB and Kindle. Book excerpt: An exploratory investigation has been made at Mach numbers from 0.40 to 0.95 to determine the effects on lift, drag, and pitching moment of blowing a jet exhaust over the upper surface of a 50 deg swept leading-edge wing. Also investigated were the effects of varying the longitudinal and vertical location of the nozzle exit on the induced effects of jet blowing.

Download or read book Effect of Fin flare Combinations on the Aerodynamic Characteristics of a Body at Mach Numbers 1 61 and 2 20 written by Clyde Hayes and published by . This book was released on 1965 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Basic Pressure Measurements at a Mach Number of 1 43 on a Thing 45 Degree Sweptback Highly Tapered Wing with Systematic Spanwise Twist Variations written by John P. Jr Mugler and published by . This book was released on 1960 with total page 78 pages. Available in PDF, EPUB and Kindle. Book excerpt: Pressure distributions are presented on four wings: an untwisted wing to serve as a reference, and wings with linear, quadratic, and cubic twist variations along the span. All the twisted wings had 0 degrees twist at the 10-percent-semispan station and 6 degrees twist at he tip. The tests were made at a Mach number of 1.43 and covered an angle-of-attack range from -4 degrees to 20 degrees. The average Reynolds number based on the wing mean aerodynamic chord was 2.9 X 10(6) during tests at a stagnation pressure of 1.0 atmosphere and 1.5 X 10(6) during tests at a stagnation pressure of 0.5 atmosphere.

Download or read book The Effects of Body Camber on Body Pressure Distributions and Wing Forces for Mach Numbers from 2 0 to 7 6 written by Frank Herman Durgin and published by . This book was released on 1961 with total page 83 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Applied Mechanics Reviews written by and published by . This book was released on 1987 with total page 338 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Aeronautical Engineering written by and published by . This book was released on 1985 with total page 488 pages. Available in PDF, EPUB and Kindle. Book excerpt: A selection of annotated references to unclassified reports and journal articles that were introduced into the NASA scientific and technical information system and announced in Scientific and technical aerospace reports (STAR) and International aerospace abstracts (IAA).