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Tuesday, August 4, 2020 | History

3 edition of Propfan test assessment propfan propulsion system static test report found in the catalog.

Propfan test assessment propfan propulsion system static test report

Propfan test assessment propfan propulsion system static test report

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  • 35 Currently reading

Published by National Aeronautics and Space Administration, Lewis Research Center, For sale by the National Technical Information Service in Cleveland, Ohio, [Springfield, Va .
Written in English

    Subjects:
  • Turbines -- Testing.,
  • Compressors -- Blades.

  • Edition Notes

    StatementD.M. O"Rourke.
    SeriesNASA contractor report -- 179613., NASA contractor report -- NASA CR-179613.
    ContributionsLewis Research Center.
    The Physical Object
    FormatMicroform
    Pagination1 v.
    ID Numbers
    Open LibraryOL15391529M

    Back to Static Models. These photos start in with preparations for the Lockheed PTA (Propfan Test Assessment) tests on a Gulfstream Model. The photos are of the test. The final photo is looking our the roll-up door of the Jet Exit Facility where the propulsion . The Pratt & Whitney/Allison DX was an experimental aircraft engine, a hybrid between a turbofan and a turboprop known as a engine was designed in the s to power proposed propfan aircraft such as the Boeing 7J7 and the MD and MD derivatives of the McDonnell Douglas MDAs of , it is still one of only four different contra-rotating propfan .

    COVID Resources. Reliable information about the coronavirus (COVID) is available from the World Health Organization (current situation, international travel).Numerous and frequently-updated resource results are available from this ’s WebJunction has pulled together information and resources to assist library staff as they consider how to handle . noise and performance assessment methodology for advanced propfan powered aircraft con gura-tions is introduced. The approach is based on rst principles and combines a coupled aircraft and propulsion system performance analysis with 3-D unsteady, full-wheel CRP CFD computations and aero-acoustic simulations.

    Additional Physical Format: Print version: Propfan test assessment (PTA) final project report. [Washington, D.C.]: National Aeronautics and Space Administration, []. The need for improved thrust specific fuel consumption to reduce fuel burned and aircraft direct operating cost is the dominant factor. Typical cycle trends for minimizing fuel consumption are reviewed, and shp class engine configurations for propfan propulsion systems for the 's are presented.


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Propfan test assessment propfan propulsion system static test report Download PDF EPUB FB2

Propfan Test Assessment Propfan Propulsion System Static Test Report Contract NAS September [NASA-CR) PROPFAN TEST ASSESSMEN2 PROPFKN PROPULSION SYSTEM STATIC TEST K_PO_T Contractor Report, Feb.

- Jun. [Lockheed-Georgia Co.) p Avail: NTIS HC AII/MF &01 CSC_ 21£ G3/07 N Unclas Get this from a library. Propfan test assessment propfan propulsion system static test report. [D M O'Rourke; Lewis Research Center.]. Propfan test assessment propfan propulsion system static test report.

By D. Orourke. Abstract. The propfan test assessment (PTA) propulsion system successfully completed over 50 hours of extensive static ground tests, including a 36 hour endurance test. All major systems performed as expected, verifying that the large-scale m diameter Author: D.

Orourke. Hamilton Standard, the only remaining large American manufacturer of aircraft propellers, developed the propfan concept in the early s. Numerous design variations of the propfan were tested by Hamilton Standard, in conjunction with NASA in this decade.

This testing led to the Propfan Test Assessment (PTA) program, where Lockheed-Georgia proposed. Buy Propfan test assessment propfan propulsion system static test report (SuDoc NAS ) by D.

O'Rourke (ISBN:) from Amazon's Book Store. Free UK delivery Free UK delivery The eight advanced turboprop en route noises represented the NASA Propfan Test Assessment aircraft operating at different combinations of altitude.

team is currently developing a third propeller propulsion system for flight testing late this year. This is a report on the progress of one of the NASA-industry flight test programs, called the Propfan Test Assessment (PTA) Program.

Lockheed-Georgia is the prime contractor for PTA with Allison, Hamilton Standard, Rohr, Gulfstream. The DX Propfan Demonstrator Propulsion System, whose flight testing on an MD airliner testbed was recently completed, has a powerplant encompassing a gas generator developed from engines.

American Institute of Aeronautics and Astronautics Sunrise Valley Drive, Suite Reston, VA figure - lap static rotor test at wright-patterson air force base facility. figure - blade passing tone, db rohr pta propulsion system static test.

- test (pta) flight testie predicted o wind tunnel (lewis 8x6) o pta flight (mach ; 35 m propfan plane upstream downstream However, propfan engines, which are very similar to turboprop engines, can cruise at flight speeds approaching Mach. In addition BPR is quoted for turboprop and unducted fan installations because their high propulsive efficiency gives them the overall efficiency characteristics of very high bypass turbofans.

In summer at NASA Glenn Research. The objectives of the Propfan Test Assessment (PTA) Program were to validate in flight the structural integrity of large-scale propfan blades and to measure noise characteristics of the propfan in both near and far fields.

All program objectives were met or exceeded, on schedule and under budget. (LASC—Georgia) and NASA, in the final flight test phase of a hour Propfan Test Assessment (PTA) program, have completed advanced technology cabin acoustic treatment testing of a propfan propulsion system.

A modified Gulfstream Aerospace Corporation G—II business jet was used as a test bed. NASA Images Solar System Collection Ames Research Center. Brooklyn Museum. Full text of "NASA Technical Reports Server (NTRS) Advanced Turboprop Project".

Assessment of Propfan Propulsion Systems for Reduced Environmental Impact Andreas Peters Advisor: Prof. Spakovszky. Baseline CRP blade-tip vortex system: Front rotor tip-vortices and viscous wakes interacting with rear rotor contribute to interaction tone noise. The system studies include civil and military transport applications and data on the performance, noise, and operating costs of propfan aircraft design concepts.

NASA propfan projects with industry including the Propfan Test Assessment, PTA. program are also reviewed. Advanced turboprop transport aircraft 2. The LAP program is complemented by the propfan test assessment (PTA) program, which takes the large-scale propfan and mates it with a gas generator and gearbox to form a propfan propulsion system and then flight tests this system on the wing of a Gulfstream 2 testbed aircraft.

Multiple Application Propfan Study (MAPS): Advanced tactical transport This study was conducted to ascertain potential benefits of a propfan propulsion system application to a blended wing/body military tactical transport.

Based on a design cruise Mach no. of for the design mission, the results indicate a significant advantage in various figures of merit for the propfan.

The Propfan Test Assessment (PTA) aircraft was flown to obtain glade stress and noise data for a m (9 ft.) diameter single rotation propfan.

Tests were performed at Mach numbers to and altitudes to 12,m (40, ft.). propeller propulsion system for flight testing early in This report covers, in particular, the progress of the NASA-sponsored Propfan Test Assess-ment (PTA) flight test program.

Lockheed-Georgia is the prime contractor for PTA with Allison, Hamilton Standard, Rohr, Gulfstream, and Lockheed-California serving as major subcontractors.

Development and testing of cabin sidewall acoustic resonators for the reduction of cabin tone levels in propfan-powered aircraft (Report). OCLC Lay summary. Kuntz, H. L.; Gatineau, R. (May ). Laboratory test and acoustic analysis of cabin treatment for Propfan Test Assessment aircraft (Report).

OCLC Lay summary. A propfan' or open rotor engine is a type of aircraft engine related in concept to both the turboprop and turbofan, but distinct from both.

The European Aviation Safety Agency defines it as "A.An aircraft cabin acoustic enclosure, built in support of the Propfan Test Assessment (PTA) program, is described.

Helmholtz resonators were attached to the cabin trim panels to increase the sidewall transmission loss (TL). Resonators () .The propfan test assessment A)(PT airplane was developed y Lokheedc Aeronautical Systems Com-pany under a NASA contract to aluateev propfan structural integrit,ypropfan source noise, cabin noise and vibration, community noise related to CFR AR(F Part 36), and ground noise during en route cruise.

During ights of the APT airplane in.