3 edition of Aircraft flight flutter testing at the NASA Ames-Dryden Flight Research Facility found in the catalog.
Aircraft flight flutter testing at the NASA Ames-Dryden Flight Research Facility
M. W. Kehoe
1988 by National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility, For sale by the National Technical Information Service] in Edwards, Calif, [Springfield, Va .
Written in English
|Statement||Michael W. Kehoe.|
|Series||NASA technical memorandum -- 100417.|
|Contributions||Dryden Flight Research Facility.|
|The Physical Object|
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NASA Technical Memorandum 1 1 7 Aircraft Flight Flutter Testing at the NASA Ames-Dryden Flight Research Facility Michael W. Kehoe (6ASA-TBU 17) AIRCBAPT EL36B'I FLUTTER N TESTING AT THE kASA ACES-DBYLkE €LIGHT HESEARCA FACILX'IY (NASA) If p Title: Aircraft Flight Flutter Testing at the NASA Ames-Dryden Flight Research Facility Author: Michael W.
Kehoe Subject: H Keywords: Aeroelastic instabilities, Flutter testing Get this from a library. Aircraft flight flutter testing at the NASA Ames-Dryden Flight Research Facility.
[M W Kehoe; Dryden Flight Research Facility.] Aircraft flight flutter testing at the NASA Ames-Dryden Flight Research Facility. MICHAEL KEHOE; MICHAEL KEHOE. NASA, Flight Research Center, Edwards, CA. Search for more papers by this author Published Online: 17 Aug Journal of Aircraft, Vol.
47, No. :// 2 days ago Employed by NASA Ames-Dryden, the employee-owned group was also contracted to work on NASA's FXL flight test program.
Twenty-five years after creation, DEI has grown to several hundred employees with $20 million in annual sales and has expanded its aerodynamic analysis tech niques to justify its company claim: "Where imagination takes shape." A program conducted between and at the NASA Dryden Flight Research Center, Edwards, Calif., successfully demonstrated an aircraft wing that could be pivoted obliquely from zero to 60 degrees during flight.
The unique wing was demonstrated on a small, subsonic jet-powered research aircraft called Aircraft flight flutter testing at the NASA Ames-Dryden Flight Research Facility book AD-1 (Ames Dryden -1) Fixed Wing Model Retired (1) Ames Research Center, Dryden Flight Research Center: Dryden Flight Research Center: The NASA M2-F1 was a lightweight, unpowered prototype aircraft, developed to flight test the wingless Lifting body concept.
It looked like a "flying bathtub," and was designated the M2–F1, the "M" referring to "manned" and "F" referring to "flight" :// Abstract: The NASA Ames-Dryden Flight Research Aircraft flight flutter testing at the NASA Ames-Dryden Flight Research Facility book at Edwards, California, operates a mixed fleet of research aircraft employing nickel-cadmium (NiCd) batteries in a variety of flight-critical applications.
Dryden's Battery Systems Laboratory (BSL), a computerized facility for battery maintenance servicing, has developed over two decades AIRCRAFT FLIGHT FLUTTER TESTING AT THE NASA AMES-DRYDEN FLIGHT RESEARCHFACILITY Authors: Michael W.
Kehoe Report Number: NASA-TM Performing Organization: NASA Dryden Flight Research Center, Edwards, CA Availability: Format(s) on-line: PDF (1, KBytes) Report Date: May No.
Pages: 17 XA AIRCRAFT STRUCTURAL LOADS FLIGHT TESTING Robert Sims* NASA Ames Research Center Dryden Flight Research Facility Edwards, California and Paul McCrosson, t Robert Ryan, t and Joe Riverat Grumman Aircraft Systems Grumman Aerospace Corporation Edwards, California Abstract The XA research and technology demonstrator air- Many parameter identification techniques have been used at the NASA Ames Research Center, Dryden Flight Research Facility at Edwards Air Force Base to determine the aeroelastic stability of new and modified research vehicles in flight.
This paper presents a summary of each technique used with emphasis on fast Fourier transform :// Aircraft flight flutter testing at the NASA Ames-Dryden Flight Research Facility.
Many parameter identification techniques have been used at the NASA Ames Research Center, Dryden Research Facility at Edwards Air Force Base to determine the aeroelastic stability of new and modified research vehicles in flight. This paper presents a Aircraft flight flutter testing at the NASA Ames-Dryden Flight Research Facility book in the experiment.
For example, an F aircraft at the NASA Ames-Dryden Flight Research Facility was used to carry aloft a precision 10 cone that has been used as an international wind tunnel calibra tion device (Fig. 6 (a)). In this experiment, tran sition Reynolds number was measured in flight to During Dryden flight testing, the X aircraft established several milestones.
On November 6,the X achieved controlled flight at a degree angle of attack. On Apthe second X successfully executed a rapid minimum-radius, degree turn using a post-stall maneuver, flying well beyond the aerodynamic limits of any Abstract: A simulator evaluation of a remotely piloted research vehicle was conducted at NASA Ames Research Center's Dryden Flight Research Facility to determine the utility of a visual display when studying the influence of changes in the lateral stick gearing gains during landing approaches.
The test vehicle used in this study was a highly Performing Organization: NASA Dryden Flight Research Center, Edwards, CA Abstract: A system to calibrate airdata probes at angles of attack between 0 and 90 deg was developed and tested at the NASA Ames Dryden Flight Research Facility.
This system used a test fixture mounted to the roof of a ground vehicle and included an onboard The experimental inlet was checked out on NASA Dryden’s FB aeronautics research test bed aircraft, which continues to be an innovative and cost-effective tool for flight test of advanced Wallace, Lane E.
Flights of Discovery: 50 Years at the NASA Dryden Flight Research Center. NASA SP, Click below to view this book in a three part PDF: Part 1. Part 2. Part 3. Herring, Mack R. Way Station to Space: A History of the John C. Stennis Space Center. NASA SP, Click here to view a PDF of this HTML A research excitation system was test flown at the NASA Dryden Flight Research Facility on the two-seat FXL aircraft.
The excitation system is a wingtip-mounted Joint USAF/NASA hypersonic research aircraft study. Role of research aircraft in technology development.
Aircraft flight flutter testing at the NASA Ames-Dryden Flight Research Facility. MICHAEL KEHOE; 4th Flight Test Conference August Experimental supersonic combustion research at NASA :// A research excitation system was test flown at the NASA Dryden Flight Research Facility on the two-seat FXL aircraft.
The excitation system is a wingtip-mounted vane with a rotating slotted NASA Technical Memorandum Flutter Clearance of the FA Variable-Sweep Transition Flight Experiment Airplane-- Phase 2 Lawrence C.
Freudinger and Michael W. Kehoe NASA Ames Research Center, Dryden Flight Research Facility, Edwards, California I_IASA National Aeronautics and Space Administration Ames Research Center American Institute of Aeronautics and Astronautics Sunrise Valley Drive, Suite Reston, VA Abstract.
Over the past several years the NASA Ames-Dryden Flight Research Facility at Edwards Air Force Base has developed a variety of flight flutter and ground test techniques which have been applied to an assortment of new or modified aerospace research :// by the Dryden Flight Research Facility of NASA Ames Research Center.
tion of the flight-readiness review, the air- worthiness and flight safety review, work sched- uling, technical briefings, and preflight and postflight crew briefings. The configuration control process used on the XA program is To develop this technology base, NASA Dryden Flight Research Facility (Edwards, CA), McDonnell Aircraft Company (St.
Louis, MO), and Pratt & Whitney (West Palm Beach, FL) have developed and flight-tested an adaptive performance seeking control system which optimizes the quasi-steady-state performance of the F propulsion Each aircraft was powered by a General Electric FGE engine produc pounds of thrust.
The program was a joint effort of the Department of Defense's Defense Advanced Research Projects Agency (DARPA), the U.S. Air Force, the Ames-Dryden Flight Research Facility, the Air Force Flight Test Center, and the Grumman :// Get this from a library. Overview of the NASA Ames-Dryden integrated test facility.
[Dale A Mackall; David McBride; Dorothea Cohen; Ames Research Center.; Dryden Flight Research Facility,] -- The Integrated Test Facility (ITF), being built at the NASA Ames Research Center's Dryden Flight Research Facility (ADFRF), will provide new real-time test capabilities for emerging research An array of major research facilities and services are located at the four aeronautical Centers of Excellence -- Ames Research Center, Dryden Flight Research Center, Langley Research Center, and Lewis Research Center.
Many facilities (such as the National Transonic Facility) and expertise are unique in the U.S. and even the :// Patrick Stoliker. Deputy Director NASA Dryden Flight Research Center. On May 2, —virtually 60 years ago—36 people boarded BOAC’s De Havilland Comet DHknown as “Yoke Peter” to its crew for last letters of its registration G-ALYP, took their seats and readied for a long were the first paying passengers of the modern jet age, departing London for a 7,mile The research aircraft was an F/AA with wings modified to reduce stiffness and a new control system to increase control authority.
Aircraft flight flutter testing at the NASA Ames-Dryden Ames highlighted its new work on heat transfer at high altitude, as well as its burgeoning agenda on the performance efficiencies of swept wings. Lunch cost $, was served in the new flight research hangar, and the hangar floor was ringed with displays of new instruments and research techniques.
Brochure for the Ames :// /background-and-evolution/ames-inspection. The fixed-wing, airplane configuration flight-test results of the Rotor System Research Aircraft (RSRA), NASAat Ames/Dryden Flight Research Center are :// Guest Materials Langley Inspection Brochure () Open House Tour Pamphlet () Inspection Agenda () Invitation Packet () Photographs of NASA’s first Inspection, held at Langley in Mayemphasized the role the former NACA labs were playing in the new Office of Advanced Research and Technology (OART).
/background-and-evolution/langley-inspection. •8x6 Transonic Wind Tunnel • 9x15 Low Speed Wind Tunnel • Propulsion Systems Lab LANGLEY RESEARCH CENTER • National Transonic Facility • 8-foot High Temperature Tunnel • Langley Aerothermodynamics Lab • 14x22 Subsonic Wind Tunnel • Transonic Dynamics Tunnel • 4-foot Supersonic Unitary Tunnel • foot Vertical Spin Tunnel DRYDEN FLIGHT RESEARCH CENTER AlAA Journal of Aircraft, Vol.
18, No, 11, November3 Theordsen, T.: General Theory of Aerodynamic Instability and the Mechanism of Flutter. NACA Report4 Tolve, L.: History of Flight Flutter Testing. Proceedings of the Flight Flutter Testing Symposium.
New Printing, NASA A Perspective on 15 Years of Proof-of-Concept Aircraft Development and Flight Research at Ames-Moffett by Rotorcraft and Powered-Lift Flight Projects Division, NASA Ames Research Center, Moffett Field, CA: NASA RP, Fimmel, Richard The Earth Observer.
September - October Vol Issue 5. At approximately 5 a.m. Eastern Daylight Time on Aug NASA’s Orbital Debris Program at Johnson Space Flight Center reported that debris from the Ice, Clouds, and land Elevation Satellite (ICESat) fell to.
Earth over the Barents Sea near Marmarisk, :// Overview Ames hosted its last Inspection on July 14 Again, the dates were selected to follow the meetings of the Institute of Aeronautical The July Inspection at Ames was both the laboratory’s final Inspection and the final Inspection of the NACA :// /background-and-evolution/ames-inspection.
Overview Ames hosted a triennial inspection on June 27 The dates were selected to follow the joint meetings in Los Angeles of the Institute The talks at the June Inspection of the Ames Laboratory revealed that the more advanced aircraft of the future required the same type of NACA research as previous :// /background-and-evolution/ames-inspection.
Aircraft flight flutter testing at the NASA Ames-Dryden Flight Research Facility [microform] / Pdf W Transformations in aeroelasticity: affine similarity and reducing of aeroelasticity problems for anisot A computational transonic flutter boundary tracking procedure [microform] / J.
W. Gallman, J. T. Batina,