Download or read book Jet Effects on the Base Afterbody and Tail Regions of a Twin Engine Airplane Model with High and Low Horizontal tail Locations written by and published by . This book was released on 1959 with total page 70 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book NASA Technical Note written by and published by . This book was released on 1976 with total page 920 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book NASA Technical Memorandum written by and published by . This book was released on 1980 with total page 104 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Jet Exit and Airframe Interference Studies on Twin engine fuselage Aircraft Installations written by and published by . This book was released on 1966 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Twin Engine Attack Type Airplane Model with Large Speed Brake Thrust Spoiler Surfaces written by and published by . This book was released on 1961 with total page 64 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Interference Between Exhaust System and Afterbody of Twin engine Fuselage Configurations written by Jack F. Runckel and published by . This book was released on 1974 with total page 52 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Sting and Jet Interference Effects on the Afterbody Drag of a Twin engine Variable Sweep Fighter Model at Transonic Speeds written by and published by . This book was released on 1963 with total page 76 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Summary of Research on Jet Exit Installations written by and published by . This book was released on 1966 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Jet Interference Effects on a Model of a Single Engine Four Jet V STOL Airplane at Mach Numbers from 0 60 to 1 00 written by and published by . This book was released on 1962 with total page 34 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Afterbody Temperatures Pressures and Aerodynamic Characteristics Resulting from Extension of Speed Brake Configurations Into the Exhaust Jets of a Twin Engine Attack Type Airplane Model written by and published by . This book was released on 1961 with total page 72 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Steady Loads Due to Jet Interference on Wings Tails and Fuselages at Transonic Speeds written by John M. Swihart and published by . This book was released on 1957 with total page 20 pages. Available in PDF, EPUB and Kindle. Book excerpt: This paper gives the results of some recent investigations of jet-interference effects on actual airplane configurations at transonic speeds. Data presented herein were obtained with hot jets on both wind-tunnel and flight models. Results indicate that jet-induced effects are small at subsonic speeds; however, at low supersonic Mach numbers, these effects are comparable to those obtained at substantially higher Mach numbers.
Download or read book NASA Technical Paper written by and published by . This book was released on 1983 with total page 592 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Bibliography on Aerodynamics of Airframe engine Integration of High speed Turbine powered Aircraft Volume 1 written by and published by . This book was released on 1980 with total page 100 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book The Influence of Vertical tail Design and Direction of Propeller Rotation on Trim Characteristics of a Twin engine airplane Model with One Engine Inoperative written by Marvin Pitkin and published by . This book was released on 1945 with total page 82 pages. Available in PDF, EPUB and Kindle. Book excerpt: Summary: Tests have been made in the Langley free-flight tunnel to determine the influence of mode of propeller rotation and vertical-tail design upon the trim characteristics of a model of a twin-engine airplane with one engine inoperative. The test model was mounted on a trim stand, which allowed freedom in roll and yaw under conditions simulating those required by the NACA and the Army Air Forces for asymmetric-power operation in flight. The seven vertical-tail designs tested included three tails of low aspect ratio and of different area, one twin tail of low aspect ratio, two tails of high aspect ratio and with different rudder areas, and one all-movable tail of high aspect ratio equipped with a linked tab. All tests were made with the flaps down.
Download or read book Effect on Empennage Location on Twin engine Afterbody nozzle Aerodynamic Characteristics at Mach Numbers from 0 6 to 1 2 written by Laurence D. Leavitt and published by . This book was released on 1983 with total page 228 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Mass Injection and Jet Flow Simulation Effects on Transonic Afterbody Drag written by Wladimiro Calarese and published by . This book was released on 1978 with total page 184 pages. Available in PDF, EPUB and Kindle. Book excerpt: An experimental investigation has been performed to determine the effects of boattail injection and jet flow simulation on the afterbody drag of a slender body of revolution in the transonic regime at zero angle of attack, such as engine nacelles and boattailed afterbodies with isolated engines. A correlation between sting and jet diameter has been established. The jet plume and the nozzle pressure ratio simulators have been found appropriate and useful as a testing technique. Boattail mass injection usually produces a drag coefficient reduction and is more effective at high nozzle pressure ratios. Boattail injection is more effective if used in regions of separated flow. (Author).
Download or read book Effect of Empennage Location on Twin engine Afterbody nozzle Aerodynamic Characteristics at Mach Numbers from 0 6 to 1 2 written by Laurence D. Leavitt and published by . This book was released on 1983 with total page 230 pages. Available in PDF, EPUB and Kindle. Book excerpt:
