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Book Wind tunnel Investigation of Aerodynamic Performance  Steady and Vibratory Loads  Surface Temperatures  and Acoustic Characteristics of a Large scale Twin engine Upper surface Blown Jet flap Configuration

Download or read book Wind tunnel Investigation of Aerodynamic Performance Steady and Vibratory Loads Surface Temperatures and Acoustic Characteristics of a Large scale Twin engine Upper surface Blown Jet flap Configuration written by and published by . This book was released on 1976 with total page 208 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Wind tunnel Investigation of the Aerodynamic Performance  Steady and Vibratory Loads  Surface Temperatures and Acoustic Characteristics of a Large scale Twin engine Upper surface Blown Jet flap Configuration

Download or read book Wind tunnel Investigation of the Aerodynamic Performance Steady and Vibratory Loads Surface Temperatures and Acoustic Characteristics of a Large scale Twin engine Upper surface Blown Jet flap Configuration written by and published by . This book was released on 1975 with total page 170 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Aerodynamic Characteristics  Temperature  and Noise Measurements of a Large scale External flow Jet augmented flap Model with Turbojet Engines Operating

Download or read book Aerodynamic Characteristics Temperature and Noise Measurements of a Large scale External flow Jet augmented flap Model with Turbojet Engines Operating written by Marvin P. Fink and published by . This book was released on 1961 with total page 52 pages. Available in PDF, EPUB and Kindle. Book excerpt: An investigation has been conducted in the Langley full-scale tunnel on a large-scale model powered by turbojet engines with flattened rectangular nozzles. The wing had 35° sweep of the leading edge, an aspect ratio of 6.5, a taper ratio of 0.31, and NACA 65(1)-412 and 65-408 airfoils at the root and tip. The investigation included measurements of the longitudinal aerodynamic characteristics of the model with half-span and full-span flaps and measurements of the sound pressure and skin temperature on the portions of the lower surface of the wing immersed in the jet flow. The tests were conducted over a range or angles of attack from -8° to 16° for Reynolds numbers from 1.8 x 106 to 4.4 x 106 and a range of momentum coefficients from 0 to 2.0. In general, the aerodynamic results of this investigation made with a large-scale hot-jet model verified the results of previous investigations with small models powered by compressed-air jets. Although blowing was only done over the inboard portion of the wing, substantial amounts of induced lift were also obtained over the outboard portion of the wing. Skin temperatures were about 340° F and wing heating could be handled with available materials without cooling. Random acoustic loadings on the wing surface were high enough to indicate that fatigue failure from this source would require special consideration in the design of an external-flow jet flap system for an airplane.

Book Aspects of Investigating STOL Noise Using Large Scale Wind Tunnel Models

Download or read book Aspects of Investigating STOL Noise Using Large Scale Wind Tunnel Models written by and published by . This book was released on 1972 with total page 72 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book NASA Technical Memorandum

Download or read book NASA Technical Memorandum written by and published by . This book was released on 1975 with total page 558 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Scientific and Technical Aerospace Reports

Download or read book Scientific and Technical Aerospace Reports written by and published by . This book was released on 1978 with total page 1008 pages. Available in PDF, EPUB and Kindle. Book excerpt: Lists citations with abstracts for aerospace related reports obtained from world wide sources and announces documents that have recently been entered into the NASA Scientific and Technical Information Database.

Book V STOL Wind tunnel Testing

Download or read book V STOL Wind tunnel Testing written by and published by . This book was released on 1984 with total page 78 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Innovation in Flight

Download or read book Innovation in Flight written by Joseph R. Chambers and published by . This book was released on 2005 with total page 406 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book NASA Technical Note

Download or read book NASA Technical Note written by and published by . This book was released on 1961 with total page 778 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Monthly Catalog of United States Government Publications  Cumulative Index

Download or read book Monthly Catalog of United States Government Publications Cumulative Index written by United States. Superintendent of Documents and published by . This book was released on 1976 with total page 1408 pages. Available in PDF, EPUB and Kindle. Book excerpt: