F 15b Flight Test Fixture 2 A Test Bed For Flight Research

Download F 15b Flight Test Fixture 2 A Test Bed For Flight Research full books in PDF, epub, and Kindle. Read online F 15b Flight Test Fixture 2 A Test Bed For Flight Research ebook anywhere anytime directly on your device. Fast Download speed and no annoying ads. We cannot guarantee that every ebooks is available!

F-15b/Flight Test Fixture 2

Download F-15b/Flight Test Fixture 2 PDF Online Free

Author : National Aeronautics and Space Administration (NASA)
Publisher : Createspace Independent Publishing Platform
ISBN 13 : 9781722391713
Total Pages : 54 pages
Book Rating : 4.3/5 (917 download)

Book Synopsis F-15b/Flight Test Fixture 2 by : National Aeronautics and Space Administration (NASA)

Download or read book F-15b/Flight Test Fixture 2 written by National Aeronautics and Space Administration (NASA) and published by Createspace Independent Publishing Platform. This book was released on 2018-07-08 with total page 54 pages. Available in PDF, EPUB and Kindle. Book excerpt: NASA Dryden Flight Research Center has developed a second-generation flight test fixture for use as a generic test bed for aerodynamic and fluid mechanics research. The Flight Test Fixture 2 (FTF-2) is a low-aspect-ratio vertical fin-like shape that is mounted on the centerline of the F-I5B lower fuselage. The fixture is designed for flight research at Mach numbers to a maximum of 2.0. The FTF-2 is a composite structure with a modular configuration and removable components for functional flexibility. This report documents the flow environment of the fixture, such as surface pressure distributions and boundary-layer profiles, throughout a matrix of conditions within the F-15B/FTF-2 flight envelope. Environmental conditions within the fixture are presented to assist in the design and testing of future avionics and instrumentation. The intent of this document is to serve as a user's guide and assist in the development of future flight experiments that use the FTF-2 as a test bed. Additional information enclosed in the appendices has been included to assist with more detailed analyses, if required. Richwine, David M. Armstrong Flight Research Center...

F-15B/Flight Test Fixture 2: A Test Bed for Flight Research

Download F-15B/Flight Test Fixture 2: A Test Bed for Flight Research PDF Online Free

Author :
Publisher :
ISBN 13 :
Total Pages : 58 pages
Book Rating : 4.:/5 (317 download)

Book Synopsis F-15B/Flight Test Fixture 2: A Test Bed for Flight Research by :

Download or read book F-15B/Flight Test Fixture 2: A Test Bed for Flight Research written by and published by . This book was released on 1996 with total page 58 pages. Available in PDF, EPUB and Kindle. Book excerpt:

The F-15B Propulsion Flight Test Fixture

Download The F-15B Propulsion Flight Test Fixture PDF Online Free

Author : Stephen Corda
Publisher :
ISBN 13 :
Total Pages : 20 pages
Book Rating : 4.:/5 (317 download)

Book Synopsis The F-15B Propulsion Flight Test Fixture by : Stephen Corda

Download or read book The F-15B Propulsion Flight Test Fixture written by Stephen Corda and published by . This book was released on 2001 with total page 20 pages. Available in PDF, EPUB and Kindle. Book excerpt: The design and development of the F-15B Propulsion Flight Flight Test Fixture (PFTF), a new facility for propulsion flight research, is described. Mounted underneath an F-15B fuselage, the PFTF provides volume for experiment systems and attachment points for propulsion devices. A unique feature of the PFTF is the incorporation of a six-degree-of-freedom force balance. Three-axis forces and moments can be measured in flight for experiments mounted to the force balance. The NASA F-15B airplane is described, including its performance and capabilities as a research test bed aircraft. The detailed description of the PFTF includes the geometry, internal layour and volume, force-balance operations, available instrumentation, and allowable experiment size and weight. The aerodynamic, stability and control, and structural designs of the PFTF are discussed, included results from aerodynmaic computational fluid dynamic calculations and structural analyses.

In-Flight Vibration Environment of the NASA F-15B Flight Test Fixture

Download In-Flight Vibration Environment of the NASA F-15B Flight Test Fixture PDF Online Free

Author :
Publisher :
ISBN 13 :
Total Pages : 34 pages
Book Rating : 4.:/5 (317 download)

Book Synopsis In-Flight Vibration Environment of the NASA F-15B Flight Test Fixture by :

Download or read book In-Flight Vibration Environment of the NASA F-15B Flight Test Fixture written by and published by . This book was released on 2002 with total page 34 pages. Available in PDF, EPUB and Kindle. Book excerpt: Flight vibration data are analyzed for the NASA F- 1 5B/Flight Test Fixture 11 test bed. Understanding the in-flight vibration environment benefits design and integration of experiments on the test bed. The power spectral density (PSD) of accelerometer flight data is analyzed to quantify the in-flight vibration environment from a frequency of 15 Hz to 1325 Hz. These accelerometer data are analyzed for typical flight conditions and maneuvers. The vibration data are compared to flight-qualification random vibration test standards. The PSD levels in the lateral axis generally are greater than in the longitudinal and vertical axes and decrease with increasing frequency. At frequencies less than approximately 40 Hz, the highest PSD levels occur during takeoff and landing.

Initial Flight Tests of the NASA F-15B Propulsion Flight Test Fixture

Download Initial Flight Tests of the NASA F-15B Propulsion Flight Test Fixture PDF Online Free

Author : Nathan Palumbo
Publisher :
ISBN 13 :
Total Pages : 20 pages
Book Rating : 4.:/5 (317 download)

Book Synopsis Initial Flight Tests of the NASA F-15B Propulsion Flight Test Fixture by : Nathan Palumbo

Download or read book Initial Flight Tests of the NASA F-15B Propulsion Flight Test Fixture written by Nathan Palumbo and published by . This book was released on 2002 with total page 20 pages. Available in PDF, EPUB and Kindle. Book excerpt: Flights of the F-1513/Propulsion Flight Test Fixture (PFTF) with a Cone Drag Experiment (CDE) attached have been accomplished at NASA Dryden Flight Research Center. Mounted underneath the fuselage of an F-15B airplane, the PFTF provides volume for experiment systems and attachment points for propulsion experiments. A unique feature of the PFTF is the incorporation of a six-degree-of-freedom force balance. The force balance mounts between the PFTF and experiment and measures three forces and moments. The CDE has been attached to the force balance for envelope expansion flights. This experiment spatially and inertially simulates a large propulsion test article. This report briefly describes the F-15B airplane, the PFTF, and the force balance. A detailed description of the CDE is provided.

F-15B/Flight Test Fixture 2

Download F-15B/Flight Test Fixture 2 PDF Online Free

Author :
Publisher :
ISBN 13 :
Total Pages : pages
Book Rating : 4.:/5 (972 download)

Book Synopsis F-15B/Flight Test Fixture 2 by :

Download or read book F-15B/Flight Test Fixture 2 written by and published by . This book was released on 1997 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:

Development of a Low-aspect Ratio Fin for Flight Research Experiments

Download Development of a Low-aspect Ratio Fin for Flight Research Experiments PDF Online Free

Author : David M. Richwine
Publisher :
ISBN 13 :
Total Pages : 20 pages
Book Rating : 4.:/5 (317 download)

Book Synopsis Development of a Low-aspect Ratio Fin for Flight Research Experiments by : David M. Richwine

Download or read book Development of a Low-aspect Ratio Fin for Flight Research Experiments written by David M. Richwine and published by . This book was released on 1994 with total page 20 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Design and Evaluation of a New Boundary-layer Rake for Flight Testing

Download Design and Evaluation of a New Boundary-layer Rake for Flight Testing PDF Online Free

Author : Trong T. Bui
Publisher :
ISBN 13 :
Total Pages : 24 pages
Book Rating : 4.:/5 (317 download)

Book Synopsis Design and Evaluation of a New Boundary-layer Rake for Flight Testing by : Trong T. Bui

Download or read book Design and Evaluation of a New Boundary-layer Rake for Flight Testing written by Trong T. Bui and published by . This book was released on 2000 with total page 24 pages. Available in PDF, EPUB and Kindle. Book excerpt: A new boundary-layer rake has been designed and built for flight testing on the NASA Dryden Flight Research Center F-15B/Flight Test Fixture. A feature unique to this rake is its curved body, which allows pitot tubes to be more densely clustered in the near-wall region than conventional rakes allow. This curved rake design has a complex three-dimensional shape that requires innovative solid-modeling and machining techniques. Finite-element stress analysis of the new design shows high factors of safety. The rake has passed a ground test in which random vibration measuring 12 g rms was applied for 20 min in each of the three normal directions. Aerodynamic evaluation of the rake has been conducted in the NASA Glenn Research Center 8x6 Supersonic Wind Tunnel at Mach 0-2. The pitiot pressures from the new rake agree with conventional rake data over the range of Mach numbers tested. The boundary-layer profiles computed from the rake data have been shown to have the standard logarithmic-law profile. Skin friction values computed from the rake data using the Clauser plot method agree with the Preston tube results and the van Driest II compressible skin friction correlation to approximately plus/minus 5 percent.

In-Flight Vibration Environment of the NASA F-15b Flight Test Fixture

Download In-Flight Vibration Environment of the NASA F-15b Flight Test Fixture PDF Online Free

Author : National Aeronautics and Space Adm Nasa
Publisher : Independently Published
ISBN 13 : 9781723731594
Total Pages : 32 pages
Book Rating : 4.7/5 (315 download)

Book Synopsis In-Flight Vibration Environment of the NASA F-15b Flight Test Fixture by : National Aeronautics and Space Adm Nasa

Download or read book In-Flight Vibration Environment of the NASA F-15b Flight Test Fixture written by National Aeronautics and Space Adm Nasa and published by Independently Published. This book was released on 2018-09-15 with total page 32 pages. Available in PDF, EPUB and Kindle. Book excerpt: Flight vibration data are analyzed for the NASA F-15B/Flight Test Fixture II test bed. Understanding the in-flight vibration environment benefits design and integration of experiments on the test bed. The power spectral density (PSD) of accelerometer flight data is analyzed to quantify the in-flight vibration environment from a frequency of 15 Hz to 1325 Hz. These accelerometer data are analyzed for typical flight conditions and maneuvers. The vibration data are compared to flight-qualification random vibration test standards. The PSD levels in the lateral axis generally are greater than in the longitudinal and vertical axes and decrease with increasing frequency. At frequencies less than approximately 40 Hz, the highest PSD levels occur during takeoff and landing. Peaks in the PSD data for the test fixture occur at approximately 65, 85, 105-110, 200, 500, and 1000 Hz. The pitch-pulse and 2-g turn maneuvers produce PSD peaks at 115 Hz. For cruise conditions, the PSD level of the 85-Hz peak is greatest for transonic flight at Mach 0.9. From 400 Hz to 1325 Hz, the takeoff phase has the highest random vibration levels. The flight-measured vibration levels generally are substantially lower than the random vibration test curve.Corda, Stephen and Franz, Russell J. and Blanton, James N. and Vachon, M. Jake and DeBoer, James B.Armstrong Flight Research CenterF-15 AIRCRAFT; VIBRATION TESTS; FLIGHT TESTS; RANDOM VIBRATION; FIXTURES; POWER SPECTRA; FLIGHT CONDITIONS; STEADY STATE; AIRCRAFT MANEUVERS; ACCELEROMETERS

NASA Tech Briefs

Download NASA Tech Briefs PDF Online Free

Author :
Publisher :
ISBN 13 :
Total Pages : 960 pages
Book Rating : 4.:/5 (319 download)

Book Synopsis NASA Tech Briefs by :

Download or read book NASA Tech Briefs written by and published by . This book was released on 2003 with total page 960 pages. Available in PDF, EPUB and Kindle. Book excerpt:

The Aviation History

Download The Aviation History PDF Online Free

Author : Relly Victoria Petrescu
Publisher : BoD – Books on Demand
ISBN 13 : 3848266393
Total Pages : 218 pages
Book Rating : 4.8/5 (482 download)

Book Synopsis The Aviation History by : Relly Victoria Petrescu

Download or read book The Aviation History written by Relly Victoria Petrescu and published by BoD – Books on Demand. This book was released on 2013 with total page 218 pages. Available in PDF, EPUB and Kindle. Book excerpt: According to Aulus Gellius, Archytas, the Ancient Greek philosopher, mathematician, astronomer, statesman, and strategist, was reputed to have designed and built, around 400 BC, the first artificial, self-propelled flying device, a bird-shaped model propelled by a jet of what was probably steam, said to have actually flown some 200 metres. This machine, which its inventor called The Pigeon, may have been suspended on a wire or pivot for its flight. The 9th century Muslim Berber inventor, Abbas Ibn Firnas's glider is considered by John Harding to be the first attempt at heavier-than-air flight in aviation history. In 1010 AD an English monk, Eilmer of Malmesbury purportedly piloted a primitive gliding craft from the tower of Malmesbury Abbey. Eilmer was said to have flown over 200 yards (180 m) before landing, breaking both his legs. He later remarked that the only reason he did not fly further was because he forgot to give it a tail, and he was about to add one when his concerned Abbot forbade him any further experiments. Bartolomeu de Gusmão, Brazil and Portugal, an experimenter with early airship designs. In 1709 demonstrated a small airship model before the Portuguese court, but never succeeded with a full-scale model. Pilâtre de Rozier, Paris, France, first trip by a human in a free-flying balloon (the Montgolfière), built by Joseph-Michel and Jacques-Étienne Montgolfier, . 9 km covered in 25 minutes on October 15, 1783. (see Le Globe below for first unmanned flight, 2 months earlier) Professor Jacques Charles and Les Frères Robert, two French brothers, Anne-Jean and Nicolas-Louis, variously shared three milestones of pioneering flight: Le Globe, the first unmanned hydrogen gas balloon flew on 26 August 1783. On 1 December 1783 La Charlière piloted by Jacques Charles and Nicolas-Louis Robert made the first manned hydrogen balloon flight. In 1951, the Lockheed XFV-1 and the Convair XFY tailsitters were both designed around the Allison YT40 turboprop engine drivin

Local Flow Conditions for Propulsion Experiments on the NASA F-15b Propulsion Flight Test Fixture

Download Local Flow Conditions for Propulsion Experiments on the NASA F-15b Propulsion Flight Test Fixture PDF Online Free

Author : National Aeronautics and Space Administration (NASA)
Publisher : Createspace Independent Publishing Platform
ISBN 13 : 9781720614333
Total Pages : 34 pages
Book Rating : 4.6/5 (143 download)

Book Synopsis Local Flow Conditions for Propulsion Experiments on the NASA F-15b Propulsion Flight Test Fixture by : National Aeronautics and Space Administration (NASA)

Download or read book Local Flow Conditions for Propulsion Experiments on the NASA F-15b Propulsion Flight Test Fixture written by National Aeronautics and Space Administration (NASA) and published by Createspace Independent Publishing Platform. This book was released on 2018-06-03 with total page 34 pages. Available in PDF, EPUB and Kindle. Book excerpt: Local flow conditions were measured underneath the National Aeronautics and Space Administration F-15B airplane to support development of future experiments on the Propulsion Flight Test Fixture (PFTF). The local Mach number and flow angles were measured using a conventional air data boom on a cone-cylinder mounted under the PFTF and compared with the airplane air data nose boom measurements. At subsonic flight speeds, the airplane and PFTF Mach numbers were approximately equal. Transonic Mach number values were up to 0.1 greater at the PFTF than the airplane, which is a counterintuitive result. The PFTF local supersonic Mach numbers were as much as 0.46 less than the airplane values. The maximum local Mach number at the PFTF was approximately 1.6 at an airplane Mach number near 2.0. The PFTF local angle of attack was negative at all Mach numbers, ranging from -3 to -8 degrees. When the airplane angle of sideslip was zero, the PFTF local value was zero between Mach 0.8 and Mach 1.1, -2 degrees between Mach 1.1 and Mach 1.5, and increased from zero to 1 degree from Mach 1.5 to Mach 2.0. Airplane inlet shock waves crossed the aerodynamic interface plane between Mach 1.85 and Mach 1.90.Vachon, Michael J. and Moes, Timothy R. and Corda, StephenArmstrong Flight Research CenterFLIGHT TESTS; MACH NUMBER; ANGLE OF ATTACK; SUPERSONIC SPEED; SIDESLIP; NOSES (FOREBODIES); SHOCK WAVES; PROPULSION

The F-15b Lifting Insulating Foam Trajectory (Lift) Flight Test

Download The F-15b Lifting Insulating Foam Trajectory (Lift) Flight Test PDF Online Free

Author : National Aeronautics and Space Adm Nasa
Publisher : Independently Published
ISBN 13 : 9781723897986
Total Pages : 60 pages
Book Rating : 4.8/5 (979 download)

Book Synopsis The F-15b Lifting Insulating Foam Trajectory (Lift) Flight Test by : National Aeronautics and Space Adm Nasa

Download or read book The F-15b Lifting Insulating Foam Trajectory (Lift) Flight Test written by National Aeronautics and Space Adm Nasa and published by Independently Published. This book was released on 2018-09-21 with total page 60 pages. Available in PDF, EPUB and Kindle. Book excerpt: A series of flight tests has been performed to assess the structural survivability of space shuttle external tank debris, known as divots, in a real flight environment. The NASA F-15B research test bed aircraft carried the Aerodynamic Flight Test Fixture configured with a shuttle foam divot ejection system. The divots were released in flight at subsonic and supersonic test conditions matching points on the shuttle ascent trajectory. Very high-speed digital video cameras recorded the divot trajectories. The objectives of the flight test were to determine the structural survivability of the divots in a real flight environment, assess the aerodynamic stability of the divots, and provide divot trajectory data for comparison with debris transport models. A total of 10 flights to Mach 2 were completed, resulting in 36 successful shuttle foam divot ejections. Highspeed video was obtained at 2,000 pictures per second for all of the divot ejections. The divots that were cleanly ejected remained structurally intact. The conical frustum-shaped divots tended to aerodynamically trim in both the subsonic and supersonic free-stream flow.Corda, Stephen and Whiteman, Donald and Tseng, Ting and Machin, RicardoArmstrong Flight Research Center; Johnson Space CenterFLIGHT TESTS; FOAMS; INSULATION; F-15 AIRCRAFT; COMPUTATIONAL FLUID DYNAMICS; ASCENT TRAJECTORIES; SPACE SHUTTLES; DEBRIS; EXTERNAL TANKS; FRUSTUMS; FREE FLOW; SUBSONIC FLOW; SUPERSONIC FLOW; PHOTOGRAMMETRY; HIGH SPEED CAMERAS; FLIGHT ENVELOPES; DEGREES OF FREEDOM; PANELS; STRUCTURAL RELIABILITY; DIGITAL TO VOICE TRANSLATORS

A Review of Recent Developments in Flight Test Techniques at the Ames Research Center, Dryden Flight Research Facility

Download A Review of Recent Developments in Flight Test Techniques at the Ames Research Center, Dryden Flight Research Facility PDF Online Free

Author :
Publisher :
ISBN 13 :
Total Pages : 22 pages
Book Rating : 4.:/5 (317 download)

Book Synopsis A Review of Recent Developments in Flight Test Techniques at the Ames Research Center, Dryden Flight Research Facility by :

Download or read book A Review of Recent Developments in Flight Test Techniques at the Ames Research Center, Dryden Flight Research Facility written by and published by . This book was released on 1984 with total page 22 pages. Available in PDF, EPUB and Kindle. Book excerpt:

37th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit

Download 37th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit PDF Online Free

Author :
Publisher :
ISBN 13 :
Total Pages : 450 pages
Book Rating : 4.0/5 ( download)

Book Synopsis 37th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit by :

Download or read book 37th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit written by and published by . This book was released on 2001 with total page 450 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Ground and Flight Test Structural Excitation Using Piezoelectric Actuators

Download Ground and Flight Test Structural Excitation Using Piezoelectric Actuators PDF Online Free

Author :
Publisher :
ISBN 13 :
Total Pages : 20 pages
Book Rating : 4.:/5 (317 download)

Book Synopsis Ground and Flight Test Structural Excitation Using Piezoelectric Actuators by :

Download or read book Ground and Flight Test Structural Excitation Using Piezoelectric Actuators written by and published by . This book was released on 2002 with total page 20 pages. Available in PDF, EPUB and Kindle. Book excerpt: A flight flutter experiment at the National Aeronautics and Space Administration (NASA) Dryden Fight Research Center, Edwards, California, used an 18-inch half-span composite model called the Aerostructures Test Wing (ATW). The ATW was mounted on a centerline flight test fixture on the NASA F-15B and used distributed piezoelectric strain actuators for in-flight structural excitation. The main focus of this paper is to investigate the performance of the piezoelectric actuators and test their ability to excite the first-bending and first-torsion modes of the ATW on the ground and in-flight. On the ground, wing response resulting from piezoelectric and impact excitation was recorded and compared. The comparison shows less than a 1-percent difference in modal frequency and a 3-percent increase in damping.

Flights of Discovery

Download Flights of Discovery PDF Online Free

Author : Lane E. Wallace
Publisher :
ISBN 13 :
Total Pages : 214 pages
Book Rating : 4.3/5 ( download)

Book Synopsis Flights of Discovery by : Lane E. Wallace

Download or read book Flights of Discovery written by Lane E. Wallace and published by . This book was released on 2006 with total page 214 pages. Available in PDF, EPUB and Kindle. Book excerpt: