EBookClubs

Read Books & Download eBooks Full Online

EBookClubs

Read Books & Download eBooks Full Online

Book A Computer Program to Calculate the Longitudinal Aerodynamic Characteristics of Wing flap Configurations with Externally Blown Flaps

Download or read book A Computer Program to Calculate the Longitudinal Aerodynamic Characteristics of Wing flap Configurations with Externally Blown Flaps written by Michael R. Mendenhall and published by . This book was released on 1976 with total page 100 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Calculation of the Longitudinal Aerodynamic Characteristics of Upper surface Blown Wing flap Configurations

Download or read book Calculation of the Longitudinal Aerodynamic Characteristics of Upper surface Blown Wing flap Configurations written by Michael R. Mendenhall and published by . This book was released on 1978 with total page 88 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book A Computer Program to Calculate the Longitudinal Aerodynamic Characteristics of Wing flap Configurations with Extremely Blown Flaps

Download or read book A Computer Program to Calculate the Longitudinal Aerodynamic Characteristics of Wing flap Configurations with Extremely Blown Flaps written by M. R. Mendenhall and published by . This book was released on 1976 with total page 100 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Calculation of the Longitudinal Aerodynamic Characteristics of Upper surface Blown Wing flap Configurations

Download or read book Calculation of the Longitudinal Aerodynamic Characteristics of Upper surface Blown Wing flap Configurations written by M. R. Mendenhall and published by . This book was released on 1978 with total page 90 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Calculation of the Longitudinal Aerodynamic Characteristics of STOL Aircraft with Externally blown Jet augmented Flaps

Download or read book Calculation of the Longitudinal Aerodynamic Characteristics of STOL Aircraft with Externally blown Jet augmented Flaps written by Marnix F. E. Dillenius and published by . This book was released on 1974 with total page 204 pages. Available in PDF, EPUB and Kindle. Book excerpt: A theoretical investigation was made to develop methods for predicting the longitudinal aerodynamic characteristics of externally-blown, jet-augmented wing-flap combinations. A potential flow analysis was used to develop two models: a wing-flap lifting surface model and a high-bypass-ratio turbofan engine wake model. Use of these two models in sequence provides for calculation of the wing-flap load distribution including the influence of the engine wake. The method can accommodate multiple engines per wing panel and part-span flaps but is limited to the case where the flow and geometry of the configuration are symmetric about a vertical plane containing the wing root chord. Comparisons of predicted and measured lift and pitching moment on unswept and swept wings with one and two engines per panel and with various flap deflection angles indicate satisfactory prediction of lift and moment for flap deflections up to 30 to 40 degrees. At higher flap angles with and without power, the method begins to overpredict lift, due probably to the appearance of flow separation on the flaps.

Book A Computer Program to Calculate the Logitudinal Aerodynamic Characteristics of Wing Flap Configurations with Externally Blown Flaps

Download or read book A Computer Program to Calculate the Logitudinal Aerodynamic Characteristics of Wing Flap Configurations with Externally Blown Flaps written by R. Mendenhall and published by . This book was released on 1976 with total page 90 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Effects of Wing Leading edge Flap Deflections on Subsonic Longitudinal Aerodynamic Characteristics of a Wing fuselage Configuration with a 44 Deg Swept Wing

Download or read book Effects of Wing Leading edge Flap Deflections on Subsonic Longitudinal Aerodynamic Characteristics of a Wing fuselage Configuration with a 44 Deg Swept Wing written by and published by . This book was released on 1978 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Longitudinal Aerodynamic Characteristics of an Externally Blown Flap Powered lift Model with Several Propulsive System Simulators

Download or read book Longitudinal Aerodynamic Characteristics of an Externally Blown Flap Powered lift Model with Several Propulsive System Simulators written by Danny R. Hoad and published by . This book was released on 1974 with total page 141 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Effects of Wing Leading edge Flap Deflections on Subsonic Longitudinal Aerodynamic Characteristics of a Wing fuselage Configuration with a 44   swept Wing

Download or read book Effects of Wing Leading edge Flap Deflections on Subsonic Longitudinal Aerodynamic Characteristics of a Wing fuselage Configuration with a 44 swept Wing written by William P. Henderson and published by . This book was released on 1978 with total page 44 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 Theory of Wing Sections

Download or read book Theory of Wing Sections written by Ira H. Abbott and published by Courier Corporation. This book was released on 2012-04-26 with total page 708 pages. Available in PDF, EPUB and Kindle. Book excerpt: Concise compilation of subsonic aerodynamic characteristics of NACA wing sections, plus description of theory. 350 pages of tables.

Book Low speed Investigation of the Effects of Wing Flap Deflection and Horizontal tail Configuration on the Longitudinal Aerodynamic Characteristics of an Airplane Configuration Having Tail Surfaces Outboard of the Wing Tips

Download or read book Low speed Investigation of the Effects of Wing Flap Deflection and Horizontal tail Configuration on the Longitudinal Aerodynamic Characteristics of an Airplane Configuration Having Tail Surfaces Outboard of the Wing Tips written by William C. Jr Hayes and published by . This book was released on 1960 with total page 42 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 1980 with total page 1280 pages. Available in PDF, EPUB and Kindle. Book excerpt: