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Book Additional Noise Data on the SR 3 Propeller

Download or read book Additional Noise Data on the SR 3 Propeller written by James H. Dittmar and published by . This book was released on 1981 with total page 20 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Noise of the SR 3 Propeller Model at 2 Deg and 4 Deg Angle of Attack

Download or read book Noise of the SR 3 Propeller Model at 2 Deg and 4 Deg Angle of Attack written by and published by . This book was released on 1981 with total page 34 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Noise of the 10 bladed  40 Deg Swept SR 6 Propeller in a Wind Tunnel

Download or read book Noise of the 10 bladed 40 Deg Swept SR 6 Propeller in a Wind Tunnel written by and published by . This book was released on 1982 with total page 92 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Scientific and Technical Aerospace Reports

Download or read book Scientific and Technical Aerospace Reports written by and published by . This book was released on 1992 with total page 316 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book NASA Technical Paper

Download or read book NASA Technical Paper written by and published by . This book was released on 1990 with total page 728 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Cruise Noise of the Sr 2 Propeller Model in a Wind Tunnel

Download or read book Cruise Noise of the Sr 2 Propeller Model in a Wind Tunnel written by National Aeronautics and Space Administration (NASA) and published by Createspace Independent Publishing Platform. This book was released on 2018-07 with total page 30 pages. Available in PDF, EPUB and Kindle. Book excerpt: Noise data on the SR-2 model propeller were taken in the NASA Lewis Research Center 8- by 6-Foot Wind Tunnel. The maximum blade passing tone rises with increasing helical tip Mach number to a peak level at a helical tip Mach number of about 1.05; then it remains the same or decreases at higher helical tip Mach numbers. This behavior, which has been observed with other propeller models, points to the possibility of using higher propeller tip speeds to limit airplane cabin noise while maintaining high flight speed and efficiency. Noise comparisons of the straight-blade SR-2 propeller and the swept-blade SR-7A propeller showed that the tailored sweep of the SR-7A appears to be the cause of both lower peak noise levels and a slower noise increase with increasing helical tip Mach number. Dittmar, James H. Glenn Research Center RTOP 535-03-01...

Book Cruise Noise of the SR 2 Propeller Model in a Wind Tunnel

Download or read book Cruise Noise of the SR 2 Propeller Model in a Wind Tunnel written by and published by . This book was released on 1989 with total page 32 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Noise of the SR 6 Propeller Model at 2 Deg and 4 Deg Angles of Attack

Download or read book Noise of the SR 6 Propeller Model at 2 Deg and 4 Deg Angles of Attack written by and published by . This book was released on 1983 with total page 22 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Directivity and Trends of Noise Generated by a Propeller in a Wake

Download or read book Directivity and Trends of Noise Generated by a Propeller in a Wake written by P. J. W. Block and published by . This book was released on 1986 with total page 68 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Tone Noise of Three Supersonic Helical Tip Speed Propellers in a Wind Tunnel

Download or read book Tone Noise of Three Supersonic Helical Tip Speed Propellers in a Wind Tunnel written by James H. Dittmar and published by . This book was released on 1979 with total page 62 pages. Available in PDF, EPUB and Kindle. Book excerpt: Three eight bladed supersonic helical tip speed propellers were tested in the NASA Lewis Wind Tunnel at through flow Mach numbers of 0.6, 0.7, 0.75, 0.8, and 0.85. Such propellers are being considered as propulsors for a future energy conservative aircraft. The three propellers of equal performance, incorporate different plan forms and different amounts of sweep in order to investigate their noise generation, which could cause a cabin environment problem. The acoustically designed propeller SR-3 had 45 deg of tip sweep and was significantly quieter at Mach 0.8 cruise than the straight bladed propeller, SR-2. An intermediate 30 deg tip sweep propeller, SR-1m exhibited a noise level between the other two. Enhanced pressure-time traces indicated that SR-2 and SR-1m exhibited shock-like pressure traces at Mach-0.8 cruise while the SR-3 did not. Noise trends with varying helical tip Mach number and blade loading were also observed.

Book Aeroacoustics of Flight Vehicles

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:

Book NASA Conference Publication

Download or read book NASA Conference Publication written by and published by . This book was released on 1980 with total page 800 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Popular Science

    Book Details:
  • Author :
  • Publisher :
  • Release : 1985-03
  • ISBN :
  • Pages : 120 pages

Download or read book Popular Science written by and published by . This book was released on 1985-03 with total page 120 pages. Available in PDF, EPUB and Kindle. Book excerpt: Popular Science gives our readers the information and tools to improve their technology and their world. The core belief that Popular Science and our readers share: The future is going to be better, and science and technology are the driving forces that will help make it better.

Book In flight Near  and Far field Acoustic Data Measured on the Propfan Test Assessment  PTA  Testbed and with an Adjacent Aircraft

Download or read book In flight Near and Far field Acoustic Data Measured on the Propfan Test Assessment PTA Testbed and with an Adjacent Aircraft written by Richard P. Woodward and published by . This book was released on 1993 with total page 161 pages. Available in PDF, EPUB and Kindle. Book excerpt: