Download or read book Performance and Stall Limits of a YTF30 P 1 Turbofan Engine with Uniform Inlet Flow written by and published by . This book was released on 1969 with total page 46 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Performance and Stall Limits of a YTF30 P 1 Turbofan Engine with Uniform Inlet Flow written by Willis M. Braithwaite and published by . This book was released on 1969 with total page 82 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Performance and Stall Limits of a YTF30 P 1 Turbofan Engine with Uniformed Inlet Flow written by Willis M. Braithwaite and published by . This book was released on 1969 with total page 38 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Scientific and Technical Aerospace Reports written by and published by . This book was released on 1969 with total page 464 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.
Download or read book NASA Scientific and Technical Reports written by United States. National Aeronautics and Space Administration Scientific and Technical Information Division and published by . This book was released on 1970 with total page 966 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book A Selected Listing of NASA Scientific and Technical Reports written by United States. National Aeronautics and Space Administration. Scientific and Technical Information Division and published by . This book was released on 1970 with total page 962 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book NASA Scientific and Technical Reports and Publications for 1969 A Selected Listing written by United States. National Aeronautics and Space Administration. Scientific and Technical Information Division and published by . This book was released on 1970 with total page 956 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book An Investigation of Two Variations of the Gas Generator Method to Calculate the Thrust of the Afterburning Turbofan Engines Installed in an F 111A Airplane written by Frank W. Burcham and published by . This book was released on 1971 with total page 36 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 1974 with total page 1070 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book pt III and IV written by Oak Ridge National Laboratory and published by . This book was released on 1974 with total page 508 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 1970 with total page 742 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Some Limitations on the Use of Damping in Short Pressure Points written by Ted W. Nyland and published by . This book was released on 1971 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt: The analytical study described in this report examines changes in the useful frequency response of short pressure probes resulting from variations in the viscous damping within the probe tube. The study is based on the use of the Bergh and Tijdeman recursion formula, which was modified to allow the addition of arbitrary amounts of viscous loss in any tube section. Results show that the useful response range can be increased with damping but is dependent on the operating temperature and pressure levels. At 300 K, only a 15-percent variation in average pressure is allowable if the useful response is to be a factor of three higher than that of an undamped probe. This variation increases to 20 or 30 percent at temperatures above 600 K. A computer program based on the modified recursion formula is given in an appendix.
Download or read book Performance and Stall Limits of an Afterburner equipped Turbofan Engine with and Without Inlet Flow Distortion written by Roger A. Werner and published by . This book was released on 1970 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book U S Government Research Development Reports written by and published by . This book was released on 1969-10 with total page 784 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book AIAA 74 201 AIAA 74 236 With omissions in numbering written by and published by . This book was released on 1974 with total page 442 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Research and Engineering Studies and Analyses of Fan Engine Stall written by B. H. Goethert and published by . This book was released on 1970 with total page 904 pages. Available in PDF, EPUB and Kindle. Book excerpt: The objectives of this research and engineering program are related to the performance and operational problems of augmented turbofan engines in high-speed flight. The various areas investigated are: Distorted and unsteady flow effects on axial flow compressor and stall characteristics; Data handling and analysis techniques; Investigations on other dynamic aspects of engines.
Download or read book Performance and Stall Limits of an Afterburner equipped Turbofan Engine with and Without Inlet Flow Distortion written by Roger A. Werner and published by . This book was released on 1970 with total page 46 pages. Available in PDF, EPUB and Kindle. Book excerpt:
