Download or read book Commercial Aircraft Noise Definition L 1011 TriStar written by Lockheed-California Company and published by . This book was released on 1974 with total page 280 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Commercial Aircraft Noise Definition L 1011 Tristar written by Nathan Shapiro and published by . This book was released on 1974 with total page 92 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Commercial Aircraft Noise Definition L 1011 Tristar Volume 2 L 1011 1 Data written by and published by . This book was released on 1974 with total page 305 pages. Available in PDF, EPUB and Kindle. Book excerpt: Calculation procedures to describe airplane noise during takeoff and approach have been programmed for batch operation on a large digital computer. Three routines are included. The first normalizes far-field noise spectra to reference conditions and then determines spectra at various distances from the airplane, for airport elevations between sea level and 6000 feet and ambient temperatures between 30 deg F and 100 deg F. Overall sound pressure levels, A-weighted noise levels, perceived noise levels, and effective perceived noise levels are calculated. The second routine uses aerodynamic and engine thrust data to produce takeoff and approach flight path description. Volume 2 includes L-1011-1 noise propagation and airplane performance and samples of contours.
Download or read book FAA EQ Report 73 6 Vols written by United States. Federal Aviation Administration and published by . This book was released on 1974 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Commercial Aircraft Noise Definition L 1011 TriStar written by Lockheed-California Company and published by . This book was released on 1974 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Commercial aircraft noise definition L 1011 Tristar written by and published by . This book was released on 1974 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Commercial Aircraft Noise Definition L 1011 Tristar Volume IV Program Design Specification written by Nathan Shapiro and published by . This book was released on 1974 with total page 126 pages. Available in PDF, EPUB and Kindle. Book excerpt: Calculation procedures to describe airplane noise during takeoff and approach have been programmed for batch operation on a large digital computer. Three routines are included. The first normalizes far-field noise spectra to reference conditions and then determines spectra at various distances from the airplane, for airport elevations between sea level and 6000 feet and ambient temperatures between 30F and 100F. Overall sound pressure levels, A-weighted noise levels, perceived noise levels, and effective perceived noise levels are calculated. The second routine uses aerodynamic and engine thrust data to produce takeoff and approach flight path description. Volume 4 describes the computer program and gives instructions for its operation.
Download or read book Commercial Aircraft Noise Definition L1011 Tristar written by and published by . This book was released on 1974 with total page 86 pages. Available in PDF, EPUB and Kindle. Book excerpt: Calculation procedures to describe airplane noise during takeoff and approach have been programmed for batch operation on a large digital computer. Three routines are included. The first normalizes far-field noise spectra to reference conditions and then determines spectra at various distances from the airplane, for airport elevations between sea level and 6000 feet and ambient temperatures between 30 deg F and 100 deg F. Overall sound pressure levels, A-weighted noise levels, perceived noise levels, and effective perceived noise levels are calculated. The second routine uses aerodynamic and engine thrust data to produce takeoff and approach flight path description. The basic takeoff is at equivalent airspeed, with thrust reduction or acceleration option after gear-up. The approach is along any constant glide slope between 3 and 6 degrees at constant airspeed, with a two-segment option. The last routine combines noise propagation and flight path information to produce constant noise contour footprints. The program has been exercised on Lockheed L-1011-1 Tristar/Rolls-Royce RB. 211-22 data, providing results in EPNdB and dBA.
Download or read book Commercial Aircraft Noise Definition L 1011 Tristar Volume 3 Program User s Manual written by and published by . This book was released on 1974 with total page 106 pages. Available in PDF, EPUB and Kindle. Book excerpt: Calculation procedures to describe airplane noise during takeoff and approach have been programmed for batch operation on a large digital computer. Three routines are included. The first normalizes far-field noise spectra to reference conditions and then determines spectra at various distances from the airplane, for airport elevations between sea levels and 6000 feet and ambient temperatures between 30F and 100F. Overall sound pressure levels, A-weighted noise levels, perceived noise levels, and effective perceived noise levels are calculated. The second routine uses aerodynamic and engine thrust data to produce takeoff and approach flight path description. Volume 3 presents the logic behind the calculations and outlines the computational procedures.
Download or read book Commercial Aircraft Noise Definition L 1011 Tristar written by and published by . This book was released on 1974 with total page 266 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Commercial Aircraft Noise Definition L 1011 Tristar Volume V Computer Programmer s Manual written by Nathan Shapiro and published by . This book was released on 1974 with total page 370 pages. Available in PDF, EPUB and Kindle. Book excerpt: Calculation procedures to describe airplane noise during takeoff and approach have been programmed for batch operation on a large digital computer. Three routines are included. The first normalizes far-field noise spectra to reference conditions and then determines spectra at various distances from the airplane, for airport elevations between sea level and 6000 feet and ambient temperatures between 30F and 100F. Overall sound pressure levels, A-weighted noise levels, perceived noise levels, and effective perceived noise levels are calculated. The second routine uses aerodynamic and engine thrust data to produce takeoff and approach flight path description. Volume 5 describes the computer program and give instructions for its operation.
Download or read book Aircraft Noise Definition written by B. G. Williams and published by . This book was released on 1973 with total page 84 pages. Available in PDF, EPUB and Kindle. Book excerpt: Acoustic data acquisition and reduction systems are discussed together with analytical procedures used to derive noise characteristics of a series of Boeing aircraft types. Noise data are presented in EPNdB and dB(A) units, from takeoff to low approach thrust and for aircraft altitudes from 200 to 12,000 feet. Areas of possible data deficiency are identified and 90% confidence limits established where possible. A flight test program is proposed with the objectives of improving data accuracy and establishing confidence limits over a wide range of operating conditions.
Download or read book Aircraft Noise Definition written by Billy G. Williams and published by . This book was released on 1973 with total page 2 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Aircraft Noise Definition written by Billy G. Williams and published by . This book was released on 1973 with total page 212 pages. Available in PDF, EPUB and Kindle. Book excerpt: Technical data are presented for graphically determining takeoff, cutback, and approach performance and noise under the flightpath for various Boeing Model 737 aircraft currently in operation. Data are included for all certified flap positions and cover operations from airports from sea level to 6000 ft altitude at temperatures from 30 to 100F with winds from -10 to +30 kn over the entire operational weight range. Noise data are shown for units to EPNdB and dB(A) from takeoff to low approach thrust and for aircraft altitudes between 200 to 12,000 ft.
Download or read book Environmental Protection written by International Civil Aviation Organization. Council and published by . This book was released on 2011 with total page 228 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Aircraft Noise Definition written by Billy G. Williams and published by . This book was released on 1973 with total page 112 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Aircraft Noise Definition written by Billy G. Williams and published by . This book was released on 1973 with total page 244 pages. Available in PDF, EPUB and Kindle. Book excerpt: Technical data are presented for graphically determining takeoff, cutback, and approach performance and noise under the flightpath for various Boeing Model 727 aircraft currently in operation. Data are included for all certified flap positions and cover operations from airports from sea level to 6000 ft. altitude at temperatures from 30F to 100F. with winds from -10 to +30 kn over the entire operational weight range. Noise data are shown for units of EPNdB and dB(A) from takeoff to low approach thrust and for aircraft altitudes between 200 and 12,000 ft.