The programing language used is FORTRAN IV. A description of all main and subprograms is provided so that any user possessing a FORTRAN compiler and random access capability can adapt the program to his facility. Rotor blade surface-pressure spectra can be used by the program to calculate: (1) blade station loading spectra, (2) chordwise and/or spanwise integrated blade-loading spectra, and (3) far-field rotational noise spectra. Any of five standard inline functions describing the chordwise distribution of the blade loading can be chosen in order to study parametrically the acoustic predictions. The program output consists of both printed and graphic descriptions of the blade-loading coefficient spectra and far-field acoustic spectrum. The...
Analytic propeller noise prediction involves a sequence of computations culminating in the applicati...
With a view that rotorcraft noise should be included in the preliminary design process, a relatively...
The techniques of helicopter rotor noise prediction attempt to describe precisely the details of the...
An essential prerequisite to reducing the acoustic detectability of military rotorcraft is a better ...
Computed output graphs for blade loading and rotational noise generation by rotor stator interaction
Cover title.Includes bibliographical references (p. 109).Mode of access: Internet
Computer programs were developed for use in the analysis of sound generation by subsonic rotors. Pro...
Large wind turbines can generate both broad band and impulsive noises. These noises can be controlle...
To predict the noise fields for proposed turboprop airplanes, an existing turboprop noise code by Fa...
This paper presents a status of non-CFD aeroacoustic codes at NASA Langley Research Center for the p...
A user's manual is presented for a computer program for the calculation of discrete frequency noise ...
A computer program is presented for calculating the source location of implusive noise in helicopter...
Existing prediction techniques are compiled and described. The descriptions include input and output...
A detailed description of a computer program to calculate tilt-rotor aircraft dynamic characteristic...
Program NOISE predicts General Aviation Aircraft far-field noise levels at FAA FAR Part 36 certifica...
Analytic propeller noise prediction involves a sequence of computations culminating in the applicati...
With a view that rotorcraft noise should be included in the preliminary design process, a relatively...
The techniques of helicopter rotor noise prediction attempt to describe precisely the details of the...
An essential prerequisite to reducing the acoustic detectability of military rotorcraft is a better ...
Computed output graphs for blade loading and rotational noise generation by rotor stator interaction
Cover title.Includes bibliographical references (p. 109).Mode of access: Internet
Computer programs were developed for use in the analysis of sound generation by subsonic rotors. Pro...
Large wind turbines can generate both broad band and impulsive noises. These noises can be controlle...
To predict the noise fields for proposed turboprop airplanes, an existing turboprop noise code by Fa...
This paper presents a status of non-CFD aeroacoustic codes at NASA Langley Research Center for the p...
A user's manual is presented for a computer program for the calculation of discrete frequency noise ...
A computer program is presented for calculating the source location of implusive noise in helicopter...
Existing prediction techniques are compiled and described. The descriptions include input and output...
A detailed description of a computer program to calculate tilt-rotor aircraft dynamic characteristic...
Program NOISE predicts General Aviation Aircraft far-field noise levels at FAA FAR Part 36 certifica...
Analytic propeller noise prediction involves a sequence of computations culminating in the applicati...
With a view that rotorcraft noise should be included in the preliminary design process, a relatively...
The techniques of helicopter rotor noise prediction attempt to describe precisely the details of the...