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Book Synopsis STOL Tactical Aircraft Investigation-Externally Blown Flap. Volume 1. Configuration Definition. Supplement 1. Aerodynamic Trades of Flap and Roll Control System by :
Download or read book STOL Tactical Aircraft Investigation-Externally Blown Flap. Volume 1. Configuration Definition. Supplement 1. Aerodynamic Trades of Flap and Roll Control System written by and published by . This book was released on 1973 with total page 122 pages. Available in PDF, EPUB and Kindle. Book excerpt: Contents: Comparison of climb speeds; Comparison of roll acceleration with all engines operating; Comparison of roll acceleration with one engine inoperative; Comparison of lift loss due to maximum roll control.
Book Synopsis STOL Tactical Aircraft Investigation -- Externally Blown Flap. Volume I. Configuration Definition by :
Download or read book STOL Tactical Aircraft Investigation -- Externally Blown Flap. Volume I. Configuration Definition written by and published by . This book was released on 1973 with total page 371 pages. Available in PDF, EPUB and Kindle. Book excerpt: The basic objective of the report is to provide a broader technology base to support the development of a medium STOL Transport (MST) airplane. The work is limited to the application of the externally blown flap (EBF) powered life concept. The technology of EBF STOL aircraft is investigated through analytical studies, wind tunnel testing, flight simulator testing, and design trade studies. The results obtained include development of methods for the estimation of the aerodynamic characteristics of an EBF configuration, STOL performance estimation methods, safety margins for takeoff and landing, wind tunnel investigation of the effects of varying EBF system geometry parameters, configuration definition to meet MST requirements, trade data on performance and configuration requirement variations, flight control system mechanization trade data, handling qualities characteristics, piloting procedures, and effects of applying an air cushion landing system to the MST.
Book Synopsis STOL Tactical Aircraft Investigation - Externally Blown Flap by : Dirk J. Renselaer
Download or read book STOL Tactical Aircraft Investigation - Externally Blown Flap written by Dirk J. Renselaer and published by . This book was released on 1973 with total page 109 pages. Available in PDF, EPUB and Kindle. Book excerpt: Contents: Comparison of climb speeds; Comparison of roll acceleration with all engines operating; Comparison of roll acceleration with one engine inoperative; Comparison of lift loss due to maximum roll control.
Book Synopsis STOL Tactical Aircraft Investigation. Volume 1. Configuration Definition by :
Download or read book STOL Tactical Aircraft Investigation. Volume 1. Configuration Definition written by and published by . This book was released on 1973 with total page 157 pages. Available in PDF, EPUB and Kindle. Book excerpt: The overall objective of the design effort was to conduct a preliminary vehicle-sizing activity to establish baseline configurations for the STOL tactical aircraft investigation. These preliminary baselines were used for the takeoff and landing studies and as a point of departure for wind tunnel test planning and flight control technology activities. The lift/propulsion concepts studied were: Externally Blown Flap (EBF); Mechanical Flap plus Vectored Thrust (MF/VT); and Internally Blown Flap (IBF). The report summarizes the design activities for the three-month and six-month configuration reviews.
Book Synopsis STOL Tactical Aircraft Investigation, Externally Blown Flap. Volume 2. Design Compendium by :
Download or read book STOL Tactical Aircraft Investigation, Externally Blown Flap. Volume 2. Design Compendium written by and published by . This book was released on 1973 with total page 177 pages. Available in PDF, EPUB and Kindle. Book excerpt: The basic objective of the work reported herein was to provide a braoder technology base to support the development of a medium STOL Transport (MST) airplane. This work was limited to the application of the externally blown flap (EBF) powered lift concept. The technology of EBF STOL aircraft has been investigated through analytical studies, wind tunnel testing, flight simulator testing, and design trade studies. The results obtained include development of methods for the estimation of the aerodynamic characteristics of an EBF configuration, STOL performance estimation methods, safety margins for takeoff and landing, wind tunnel investigation of the effects of varying EBF system geometry parameters, configuration definition to meet MST requirements, trade data on performance and configuration requirement variations, flight control system mechanization trade data, handling qualities characteristics; piloting procedures, and effects of applying an air cushion landing system to the MST.
Book Synopsis STOL Tactical Aircraft Investigation - Externally Blown Flap by : Robert W. Phillips
Download or read book STOL Tactical Aircraft Investigation - Externally Blown Flap written by Robert W. Phillips and published by . This book was released on 1973 with total page 58 pages. Available in PDF, EPUB and Kindle. Book excerpt: Contents: System analyses; System characteristics comparison; Control component requirements; Handling qualities.
Book Synopsis Scientific and Technical Aerospace Reports by :
Download or read book Scientific and Technical Aerospace Reports written by and published by . This book was released on 1987 with total page 938 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis STOL Tactical Aircraft Investigation. Volume IV. Wind Tunnel Data Analysis by :
Download or read book STOL Tactical Aircraft Investigation. Volume IV. Wind Tunnel Data Analysis written by and published by . This book was released on 1973 with total page 440 pages. Available in PDF, EPUB and Kindle. Book excerpt: Force and rake information measured during 1087 hours of low speed wind tunnel testing conducted by Convair Aerospace are summarized. Over 2730 data runs were generated on 242 major configuration variables that covered the following lift/propulsion concepts: mechanical flaps plus vectored thrust, externally blown flaps, and internally blown flaps. Lift data was reduced into three basic terms: power-on to power-off lift curve slope ratio, trailing edge flap lift increment at alpha = zero degrees, and maximum lift coefficient increment due to the application of power. These relationships were evaluated as a function of blowing momentum coefficient and correlated for the effects of configurational variations (wing planform, leading and trailing edges, and nacelle location). Drag data was reduced into the form of induced drag factor, minimum profile drag, thrust recovery and then analyzed as a function of blowing momentum coefficient. The pitching moment data analysis compares the flap pitching moment increment among the various configurations. (Modified author abstract).
Book Synopsis STOL Tactical Aircraft Investigation. Volume 3. Performance Ground Rules and Methods. Book 2, Takeoff and Landing Digital Computer Program by :
Download or read book STOL Tactical Aircraft Investigation. Volume 3. Performance Ground Rules and Methods. Book 2, Takeoff and Landing Digital Computer Program written by and published by . This book was released on 1973 with total page 133 pages. Available in PDF, EPUB and Kindle. Book excerpt: The MILSTOL (MILitary STOL) takeoff and landing digital computer program was developed to compute takeoff and landing characteristics of powered- lift STOL aircraft. It calculates a point mass takeoff and/or landing for a trimmed configuration with either externally blown jet flaps, internally blown jet flaps, or mechanical flaps with vectored thrust. Contained in this report are: Discussion of assumptions and methods used in the trajectory calculations; Definition of common list variables; Definition of the input variables and sample input data for the externally blown jet flap configuration; Sample output for the externally blown flap configuration; and Program listings and flow charts. The program is written in Fortran IV for use on CDC 6000 series digital computers and requires 37 K sub 8 central memory for loading and execution.
Book Synopsis Government Reports Announcements by :
Download or read book Government Reports Announcements written by and published by . This book was released on 1974 with total page 1000 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Government Reports Index written by and published by . This book was released on 1975 with total page 1096 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Government Reports Annual Index by :
Download or read book Government Reports Annual Index written by and published by . This book was released on 1974 with total page 1088 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 1974 with total page 520 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)
Book Synopsis Government Reports Announcements & Index by :
Download or read book Government Reports Announcements & Index written by and published by . This book was released on 1979 with total page 770 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book NASA Technical Paper written by and published by . This book was released on 1988 with total page 100 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Technical Information Indexes written by and published by . This book was released on 1975 with total page 126 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Government Reports Announcements by :
Download or read book Government Reports Announcements written by and published by . This book was released on 1973 with total page 1726 pages. Available in PDF, EPUB and Kindle. Book excerpt:
