Author: Publisher:
ISBN:
Category :
Languages : en
Pages : 136
Book Description
Sonic Environment of Aircraft Structure Immersed in a Supersonic Jet Flow Stream
Author: NASA Research on Structures and Materials for Supersonic Cruise Aircraft
Author: Paul A. CooperPublisher:
ISBN:
Category : Airframes
Languages : en
Pages : 56
Book Description
"The technology and data base necessary for sound technical decisions regarding long haul supersonic cruise aircraft transportation systems are considered. The objectives and status of the research elements in the structures and materials program phase of the program are reviewed. Emphasis is placed on reductions in structural mass by research on advanced structural concepts, light-weight materials, improved loads, aeroelastic predictive techniques, and by development of efficient structural design procedures."--NTRS Web site
Scientific and Technical Aerospace Reports
Author: NASA Technical Paper
Author: NASA Reference Publication
Author: AIAA 86-1500 - AIAA 86-1549
Author: Fluctuating Loads Measured on an Over-the-wing Supersonic Jet Model
Author: Conrad M. WillisPublisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 52
Book Description
Fluctuating pressure loads on the wing and flap of an over-the-wing supersonic jet model were measured. The model was tested statically and at a Mach number of 0.1 in a small free jet to simulate forward speed. Test parameters were impingement angle, nozzle height, and flap deflection. Load levels as high as 170 db were measured at the center of the impingement region during static tests. Forward speed reduced the loading about 1 db. Load level increased with increasing impingement angle and decreasing nozzle height above the wing. The effect of flap deflection was small. When scaled to full-size aircraft conditions, the maximum amplitude of the one-third-octave fluctuating pressure spectra was about 154 db at about 160 Hz. Maximum load level occurred near the intersection of the nozzle center line with the impinged surface. Downstream of the maximum the fluctuating pressure is inversely proportional to the distance downstream of the nozzle.
Aeronautical Engineering
Author: Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 524
Book Description
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).
Proceedings of the SCAR [Supersonic Cruise Aircraft Research] Conference Held at Langley Research Center, Hampton, Virginia, November 9-12, 1976
![Proceedings of the SCAR [Supersonic Cruise Aircraft Research] Conference Held at Langley Research Center, Hampton, Virginia, November 9-12, 1976 PDF](https://books.google.com/books/content/images/frontcover/XAVSAQAAMAAJ?fife=w80-h100)
Author: Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 560
Book Description
Author: