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Error In Airspeed Measurement Due To Static Pressure Field Ahead Of An Open Nose Air Inlet Model At Transonic Speeds
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Book Synopsis Error in Airspeed Measurement Due to Static-pressure Field Ahead of an Open-nose Air-inlet Model at Transonic Speeds by : Thomas C. O'Bryan
Download or read book Error in Airspeed Measurement Due to Static-pressure Field Ahead of an Open-nose Air-inlet Model at Transonic Speeds written by Thomas C. O'Bryan and published by . This book was released on 1952 with total page 22 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Index of NACA Technical Publications by : United States. National Advisory Committee for Aeronautics
Download or read book Index of NACA Technical Publications written by United States. National Advisory Committee for Aeronautics and published by . This book was released on 1955 with total page 1338 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Report by : United States. National Advisory Committee for Aeronautics
Download or read book Report written by United States. National Advisory Committee for Aeronautics and published by . This book was released on 1955 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Annual Report - National Advisory Committee for Aeronautics by : United States. National Advisory Committee for Aeronautics
Download or read book Annual Report - National Advisory Committee for Aeronautics written by United States. National Advisory Committee for Aeronautics and published by . This book was released on 1955 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt: Includes the Committee's Technical reports no. 1-1058, reprinted in v. 1-37.
Book Synopsis Research Abstracts and Reclassification Notice by : United States. National Advisory Committee for Aeronautics
Download or read book Research Abstracts and Reclassification Notice written by United States. National Advisory Committee for Aeronautics and published by . This book was released on 1954 with total page 508 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis A Selected Listing of NASA Scientific and Technical Reports for ... by :
Download or read book A Selected Listing of NASA Scientific and Technical Reports for ... written by and published by . This book was released on 1954 with total page 818 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Research Abstracts by : United States. National Advisory Committee for Aeronautics
Download or read book Research Abstracts written by United States. National Advisory Committee for Aeronautics and published by . This book was released on with total page 442 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis A Flight Evaluation of the Longitudinal Stability Characteristics Associated with the Pitch-up of a Swept-wing Airplane in Maneuvering Flight at Transonic Speeds by : Charles E. Watkins
Download or read book A Flight Evaluation of the Longitudinal Stability Characteristics Associated with the Pitch-up of a Swept-wing Airplane in Maneuvering Flight at Transonic Speeds written by Charles E. Watkins and published by . This book was released on 1955 with total page 376 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Review of Aircraft Altitude Errors Due to Static-pressure Source and Description of Nose-boom Installations for Aerodynamic Compensation of Error by : William Gracey
Download or read book Review of Aircraft Altitude Errors Due to Static-pressure Source and Description of Nose-boom Installations for Aerodynamic Compensation of Error written by William Gracey and published by . This book was released on 1959 with total page 9 pages. Available in PDF, EPUB and Kindle. Book excerpt: Summary: A brief review of airplane altitude errors due to typical pressure installations at the fuselage nose, the wing tip, and the vertical fins is presented. A static-pressure tube designed to compensate for the position errors of fuselage-nose installations in the subsonic speed range is described. This type of tube has an ogival nose shape with the static-pressure orifices located in the low-pressure region near the tip. The results of wind-tunnel tests of these compensated tubes at two distances ahead of a model of an aircraft showed the position errors to be compensated to within 1/2 percent of the static pressure through a Mach number range up to about 1.0. This accuracy of sensing free-stream static pressure was extended up to a Mach number of about 1.15 by use of an orifice arrangement for producing approximate free-stream pressures at supersonic speeds and induced pressures for compensation of error at subsonic speeds.
Book Synopsis Measurement of Aircraft Speed and Altitude by : William Gracey
Download or read book Measurement of Aircraft Speed and Altitude written by William Gracey and published by . This book was released on 1980 with total page 328 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Flight Calibrations of Fuselage Static-pressure-vent Installations for Three Types of Transports by : Norman S. Silsby
Download or read book Flight Calibrations of Fuselage Static-pressure-vent Installations for Three Types of Transports written by Norman S. Silsby and published by . This book was released on 1962 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Review of Aircraft Altitude Errors Due to Static-pressure Source and Description of Nose-boom Installations for Aerodynamic Compensation of Error by : William Gracey
Download or read book Review of Aircraft Altitude Errors Due to Static-pressure Source and Description of Nose-boom Installations for Aerodynamic Compensation of Error written by William Gracey and published by . This book was released on 1959 with total page 9 pages. Available in PDF, EPUB and Kindle. Book excerpt: A brief review of airplane altitude errors due to typical pressure installations at the fuselage nose, the wing tip, and the vertical fins is presented. A static-pressure tube designed to compensate for the position errors of fuselage-nose installations in the subsonic speed range is described. This type of tube has an ogival nose shape with the static-pressure orifices located in the low-pressure region near the tip. The results of wind-tunnel tests of these compensated tubes at two distances ahead of a model of an aircraft showed the position errors to be compensated to within 1/2 percent of the static pressure through a Mach number range up to about 1.0. This accuracy of sensing free-stream static pressure was extended up to a Mach number of about 1.15 by use of an orifice arrangement for producing approximate free-stream pressures at supersonic speeds and induced pressures for compensation of error at subsonic speeds.
Book Synopsis High-speed Wind Tunnels by : Luigi Crocco
Download or read book High-speed Wind Tunnels written by Luigi Crocco and published by . This book was released on 1946 with total page 236 pages. Available in PDF, EPUB and Kindle. Book excerpt: The importance assumed in recent times by experimental supersonic wind tunnels, as well as the power required, has brought about the need for a study which would permit a comparison of the types tested and the principal theoretical plans.
Book Synopsis Introduction to Aircraft Flight Mechanics by : Thomas R. Yechout
Download or read book Introduction to Aircraft Flight Mechanics written by Thomas R. Yechout and published by AIAA. This book was released on 2003 with total page 666 pages. Available in PDF, EPUB and Kindle. Book excerpt: Based on a 15-year successful approach to teaching aircraft flight mechanics at the US Air Force Academy, this text explains the concepts and derivations of equations for aircraft flight mechanics. It covers aircraft performance, static stability, aircraft dynamics stability and feedback control.
Book Synopsis Measurement of Aircraft Speed and Altitude by : William Gracey
Download or read book Measurement of Aircraft Speed and Altitude written by William Gracey and published by John Wiley & Sons. This book was released on 1981 with total page 288 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Flight Stability and Automatic Control by : Robert C. Nelson
Download or read book Flight Stability and Automatic Control written by Robert C. Nelson and published by WCB/McGraw-Hill. This book was released on 1998 with total page 441 pages. Available in PDF, EPUB and Kindle. Book excerpt: The second edition of Flight Stability and Automatic Control presents an organized introduction to the useful and relevant topics necessary for a flight stability and controls course. Not only is this text presented at the appropriate mathematical level, it also features standard terminology and nomenclature, along with expanded coverage of classical control theory, autopilot designs, and modern control theory. Through the use of extensive examples, problems, and historical notes, author Robert Nelson develops a concise and vital text for aircraft flight stability and control or flight dynamics courses.
Book Synopsis The Smell of Kerosene by : National Aeronautics and Space Administration
Download or read book The Smell of Kerosene written by National Aeronautics and Space Administration and published by Good Press. This book was released on 2023-12-28 with total page 279 pages. Available in PDF, EPUB and Kindle. Book excerpt: The Smell of Kerosene: A Test Pilot's Odyssey encapsulates the daring and the danger inherent in the uncharted territories of early space and aircraft testing. The collection stands as a testimonial to the evolution of aeronautics, narrating the exhilarating experiences of test pilots and their indispensable role in shaping modern aviation and space exploration. Through a compilation of memoirs, technical reports, and firsthand accounts, the anthology presents a rich tapestry of literary styles, from the methodical precision of technical writing to the deeply personal and reflective tales of peril and perseverance. This diversity underscores the anthology's broader theme - the human spirit's unyielding quest for knowledge and conquest of the skies. The contributors, primarily from the National Aeronautics and Space Administration alongside notable figures like Donald L. Mallick and Peter W. Merlin, bring a wealth of experience and insight. Their backgrounds, ranging from engineering and test piloting to aerospace history, provide a comprehensive overview of the historical and technological context of air and space exploration. Their collective narratives not only honor the legacy of the fields pioneers but also highlight the interdisciplinary nature of aeronautics, where science meets human daring. The Smell of Kerosene is a must-read for anyone fascinated by the interface between human ambition and technological progress. It offers readers a unique opportunity to engage with the personal triumphs and challenges of those who have pushed the boundaries of what was technologically possible. This anthology serves not only as an educational resource but also as a source of inspiration, urging readers to contemplate the vastness of human achievement through the prism of aeronautics and space exploration. It invites a diverse audience, from academicians to enthusiasts, to dive into the depths of this pivotal era in aerospace history.
