F/A-18A Inlet Flow Characteristics During Maneuvers with Rapidly Changing Angle of Attack

Download F/A-18A Inlet Flow Characteristics During Maneuvers with Rapidly Changing Angle of Attack PDF Online Free

Author :
Publisher :
ISBN 13 :
Total Pages : 26 pages
Book Rating : 4.:/5 (317 download)

DOWNLOAD NOW!


Book Synopsis F/A-18A Inlet Flow Characteristics During Maneuvers with Rapidly Changing Angle of Attack by :

Download or read book F/A-18A Inlet Flow Characteristics During Maneuvers with Rapidly Changing Angle of Attack written by and published by . This book was released on 1997 with total page 26 pages. Available in PDF, EPUB and Kindle. Book excerpt:

F/A-18A Inlet Flow Characteristics During Maneuvers with Rapidly Changing Angle of Attack

Download F/A-18A Inlet Flow Characteristics During Maneuvers with Rapidly Changing Angle of Attack PDF Online Free

Author :
Publisher :
ISBN 13 :
Total Pages : 18 pages
Book Rating : 4.:/5 (73 download)

DOWNLOAD NOW!


Book Synopsis F/A-18A Inlet Flow Characteristics During Maneuvers with Rapidly Changing Angle of Attack by : Andrew J. Yuhas

Download or read book F/A-18A Inlet Flow Characteristics During Maneuvers with Rapidly Changing Angle of Attack written by Andrew J. Yuhas and published by . This book was released on 1997 with total page 18 pages. Available in PDF, EPUB and Kindle. Book excerpt: The performance and distortion levels of the right inlet of the F/A-18A High Alpha Research Vehicle were assessed during maneuvers with rapidly changing angle-of-attack at the NASA Dryden Flight Research Center, Edwards, California. The distortion levels were compared with those produced by current inlet-engine compatibility evaluation techniques. The objective of these analyses was to determine whether the results obtained for steady aerodynamic conditions were adequate to describe the inlet-generated distortion levels that occur during rapid aircraft maneuvers. The test data were obtained during 46 dynamic maneuvers at Mach numbers of 0.3 and 0.4. Levels of inlet recovery, peak dynamic circumferential distortion, and peak dynamic radial distortion of dynamic maneuvers for a General Electric F404-GE-400 turbofan engine were compared with estimations based on steady aerodynamic conditions. The comparisons were performed at equivalent angle-of-attack, angle-of-sideslip, and Mach number. Results showed no evidence of peak inlet distortion levels being elevated by dynamic maneuver conditions at high angle-of-attack compared with steady aerodynamic estimations. During sweeps into high angle-of-attack, the peak distortion levels of the dynamic maneuvers rarely rose to steady aerodynamic estimations. The dynamic maneuvers were shown to be effective at identifying conditions when discrete changes in inlet behavior occur.

F/A-18a Inlet Flow Characteristics During Maneuvers with Rapidly Changing Angle of Attack

Download F/A-18a Inlet Flow Characteristics During Maneuvers with Rapidly Changing Angle of Attack PDF Online Free

Author :
Publisher : Createspace Independent Publishing Platform
ISBN 13 : 9781722226565
Total Pages : 24 pages
Book Rating : 4.2/5 (265 download)

DOWNLOAD NOW!


Book Synopsis F/A-18a Inlet Flow Characteristics During Maneuvers with Rapidly Changing Angle of Attack by : National Aeronautics and Space Administration (NASA)

Download or read book F/A-18a Inlet Flow Characteristics During Maneuvers with Rapidly Changing Angle of Attack written by National Aeronautics and Space Administration (NASA) and published by Createspace Independent Publishing Platform. This book was released on 2018-07-03 with total page 24 pages. Available in PDF, EPUB and Kindle. Book excerpt: The performance and distortion levels of the right inlet of the F/A-18A High Alpha Research Vehicle were assessed during maneuvers with rapidly changing angle-of-attack at the NASA Dryden Flight Research Center, Edwards, California. The distortion levels were compared with those produced by current inlet-engine compatibility evaluation techniques. The objective of these analyses was to determine whether the results obtained for steady aerodynamic conditions were adequate to describe the inlet-generated distortion levels that occur during rapid aircraft maneuvers. The test data were obtained during 46 dynamic maneuvers at Mach numbers of 0.3 and 0.4. Levels of inlet recovery, peak dynamic circumferential distortion, and peak dynamic radial distortion of dynamic maneuvers for a General Electric F404-GE-400 turbofan engine were compared with estimations based on steady aerodynamic conditions. The comparisons were performed at equivalent angle-of-attack, angle-of-sideslip, and Mach number. Results showed no evidence of peak inlet distortion levels being elevated by dynamic maneuver conditions at high angle-of-attack compared with steady aerodynamic estimations. During sweeps into high angle-of-attack, the peak distortion levels of the dynamic maneuvers rarely rose to steady aerodynamic estimations. The dynamic maneuvers were shown to be effective at identifying conditions when discrete changes in inlet behavior occur. Yuhas, Andrew J. and Steenken, William G. and Williams, John G. and Walsh, Kevin R. Armstrong Flight Research Center; Glenn Research Center NAS3-26617; RTOP 505-68-30...

Factors Affecting Inlet-Engine Compatibility During Aircraft Departures at High Angle of Attack for an F/A -18A Aircraft

Download Factors Affecting Inlet-Engine Compatibility During Aircraft Departures at High Angle of Attack for an F/A -18A Aircraft PDF Online Free

Author :
Publisher :
ISBN 13 :
Total Pages : 204 pages
Book Rating : 4.:/5 (317 download)

DOWNLOAD NOW!


Book Synopsis Factors Affecting Inlet-Engine Compatibility During Aircraft Departures at High Angle of Attack for an F/A -18A Aircraft by :

Download or read book Factors Affecting Inlet-Engine Compatibility During Aircraft Departures at High Angle of Attack for an F/A -18A Aircraft written by and published by . This book was released on 1999 with total page 204 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Fifty Years of Flight Research

Download Fifty Years of Flight Research PDF Online Free

Author :
Publisher :
ISBN 13 :
Total Pages : 526 pages
Book Rating : 4.:/5 (317 download)

DOWNLOAD NOW!


Book Synopsis Fifty Years of Flight Research by : David F. Fisher

Download or read book Fifty Years of Flight Research written by David F. Fisher and published by . This book was released on 1999 with total page 526 pages. Available in PDF, EPUB and Kindle. Book excerpt: A bibliography of Technical Reports from Dryden Research Center, 1946-1996. Dryden was a National Advisory Committee for Aeronautics (NACA) facility from to 1946-1958, when NACA became NASA (National Aeronautics and Space Administration). This bibliography encompasses both NACA and NASA publications. Illustrated with diagrams and photos. Black and white version.

34th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit

Download 34th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit PDF Online Free

Author :
Publisher :
ISBN 13 :
Total Pages : 548 pages
Book Rating : 4.0/5 ( download)

DOWNLOAD NOW!


Book Synopsis 34th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit by :

Download or read book 34th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit written by and published by . This book was released on 1998 with total page 548 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Monthly Catalog of United States Government Publications

Download Monthly Catalog of United States Government Publications PDF Online Free

Author :
Publisher :
ISBN 13 :
Total Pages : 892 pages
Book Rating : 4.3/5 (243 download)

DOWNLOAD NOW!


Book Synopsis Monthly Catalog of United States Government Publications by :

Download or read book Monthly Catalog of United States Government Publications written by and published by . This book was released on 1999 with total page 892 pages. Available in PDF, EPUB and Kindle. Book excerpt:

International Aerospace Abstracts

Download International Aerospace Abstracts PDF Online Free

Author :
Publisher :
ISBN 13 :
Total Pages : 980 pages
Book Rating : 4.F/5 ( download)

DOWNLOAD NOW!


Book Synopsis International Aerospace Abstracts by :

Download or read book International Aerospace Abstracts written by and published by . This book was released on 1998 with total page 980 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Aeronautical Engineering

Download Aeronautical Engineering PDF Online Free

Author :
Publisher :
ISBN 13 :
Total Pages : 348 pages
Book Rating : 4.:/5 (31 download)

DOWNLOAD NOW!


Book Synopsis Aeronautical Engineering by :

Download or read book Aeronautical Engineering written by and published by . This book was released on 1981 with total page 348 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).

NASA SP.

Download NASA SP. PDF Online Free

Author :
Publisher :
ISBN 13 :
Total Pages : 128 pages
Book Rating : 4.:/5 (3 download)

DOWNLOAD NOW!


Book Synopsis NASA SP. by :

Download or read book NASA SP. written by and published by . This book was released on 1962 with total page 128 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Beyond Tube-and-Wing

Download Beyond Tube-and-Wing PDF Online Free

Author :
Publisher :
ISBN 13 : 9781626830592
Total Pages : pages
Book Rating : 4.8/5 (35 download)

DOWNLOAD NOW!


Book Synopsis Beyond Tube-and-Wing by : Bruce Larrimer

Download or read book Beyond Tube-and-Wing written by Bruce Larrimer and published by . This book was released on 2020-06-15 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:

Aeroacoustics of Flight Vehicles

Download Aeroacoustics of Flight Vehicles PDF Online Free

Author :
Publisher :
ISBN 13 :
Total Pages : 620 pages
Book Rating : 4.F/5 ( download)

DOWNLOAD NOW!


Book Synopsis Aeroacoustics of Flight Vehicles by : Harvey H. Hubbard

Download or read book Aeroacoustics of Flight Vehicles written by Harvey H. Hubbard and published by . This book was released on 1991 with total page 620 pages. Available in PDF, EPUB and Kindle. Book excerpt:

The Smell of Kerosene

Download The Smell of Kerosene PDF Online Free

Author :
Publisher : Good Press
ISBN 13 :
Total Pages : 275 pages
Book Rating : 4.8/5 (596 download)

DOWNLOAD NOW!


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 275 pages. Available in PDF, EPUB and Kindle. Book excerpt: This book puts the reader in the pilot's seat for a "day at the office" unlike any other. The Smell of Kerosene tells the dramatic story of a NASA research pilot who logged over 11,000 flight hours in more than 125 types of aircraft. Donald Mallick gives the reader fascinating first-hand description of his early naval flight training, carrier operations, and his research flying career with NASA. After transferring to the NASA Flight Research Center, Mallick became involved with projects that further pushed the boundaries of aerospace technology. These included the giant delta-winged XB-70 supersonic airplane, the wingless M2-F1 lifting body vehicle, and triple-sonic YF-12 Blackbird. Mallick also test flew the Lunar Landing Research Vehicle and helped develop techniques used in training astronauts to land on the Moon.

Flying beyond the stall

Download Flying beyond the stall PDF Online Free

Author :
Publisher :
ISBN 13 : 9781626830196
Total Pages : 409 pages
Book Rating : 4.8/5 (31 download)

DOWNLOAD NOW!


Book Synopsis Flying beyond the stall by : Douglas A. Joyce

Download or read book Flying beyond the stall written by Douglas A. Joyce and published by . This book was released on 2014 with total page 409 pages. Available in PDF, EPUB and Kindle. Book excerpt: The X-31 Enhanced Fighter Maneuverability Demonstrator was unique among experimental aircraft. A joint effort of the United States and Germany, the X-31 was the only X-plane to be designed, manufactured, and flight tested as an international collaboration. It was also the only X-plane to support two separate test programs conducted years apart, one administered largely by NASA and the other by the U.S. Navy, as well as the first X-plane ever to perform at the Paris Air Show. Flying Beyond the Stall begins by describing the government agencies and private-sector industries involved in the X-31 program, the genesis of the supermaneuverability concept and its initial design breakthroughs, design and fabrication of two test airframes, preparation for the X-31's first flight, and the first flights of Ship #1 and Ship #2. Subsequent chapters discuss envelope expansion, handling qualities (especially at high angles of attack), and flight with vectored thrust. The book then turns to the program's move to NASA's Dryden Flight Research Center and actual flight test data. Additional tasking, such as helmet-mounted display evaluations, handling quality studies, aerodynamic parameter estimation, and a "tailless" study are also discussed.The book describes how, in the aftermath of a disastrous accident with Ship #1 in 1995, Ship #2 was prepared for its outstanding participation in the Paris Air Show. The aircraft was then shipped back to Edwards AFB and put into storage until the late 1990s, when it was refurbished for participation in the U. S. Navy's VECTOR program. The book ends with a comprehensive discussion of lessons learned and includes an Appendix containing detailed information.

Innovation in Flight

Download Innovation in Flight PDF Online Free

Author :
Publisher :
ISBN 13 :
Total Pages : 406 pages
Book Rating : 4.3/5 ( download)

DOWNLOAD NOW!


Book Synopsis Innovation in Flight by : Joseph R. Chambers

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:

The Encyclopedia of Aerodynamics

Download The Encyclopedia of Aerodynamics PDF Online Free

Author :
Publisher : Andrews UK Limited
ISBN 13 : 1785383248
Total Pages : 677 pages
Book Rating : 4.7/5 (853 download)

DOWNLOAD NOW!


Book Synopsis The Encyclopedia of Aerodynamics by : Frank Hitchens

Download or read book The Encyclopedia of Aerodynamics written by Frank Hitchens and published by Andrews UK Limited. This book was released on 2015-11-25 with total page 677 pages. Available in PDF, EPUB and Kindle. Book excerpt: The Encyclopedia of Aerodynamics was written for pilots at all levels from private pilot to airline pilot, military pilots and students of aerodynamics as a complete reference manual to aerodynamic terminology. General aerodynamic text books for pilots are relatively limited in their scope while aerodynamic text books for engineering students involve complex calculus. The references in this book, The Encyclopedia of Aerodynamics, are clearly described and only basic algebra is used in a few references but is completely devoid of any calculus - an advantage to many readers. Over 1400 references are included with alternative terms used where appropriate and cross-referenced throughout. The text is illustrated with 178 photographs and 96 diagrams. The Encyclopedia of Aerodynamics is an ideal aerodynamic reference manual for any pilot's bookshelf.

Computers Take Flight: A History of NASA's Pioneering Digital Fly-By-Wire Project

Download Computers Take Flight: A History of NASA's Pioneering Digital Fly-By-Wire Project PDF Online Free

Author :
Publisher :
ISBN 13 :
Total Pages : 210 pages
Book Rating : 4.:/5 (317 download)

DOWNLOAD NOW!


Book Synopsis Computers Take Flight: A History of NASA's Pioneering Digital Fly-By-Wire Project by : James E. Tomayko

Download or read book Computers Take Flight: A History of NASA's Pioneering Digital Fly-By-Wire Project written by James E. Tomayko and published by . This book was released on 2000 with total page 210 pages. Available in PDF, EPUB and Kindle. Book excerpt: