Variations in the Sonic Boom Pressure Signature Due to Atmospheric Conditions and Ground Reflections
Author :
Publisher :
Page : 0 pages
File Size : 40,99 MB
Release : 1969
Category :
ISBN :
A Summary of Results on Sonic-boom Pressure-signature Variations Associated with Atmospheric Conditions
Author : I. E. Garrick
Publisher :
Page : 34 pages
File Size : 27,88 MB
Release : 1968
Category : Aerodynamics, Supersonic
ISBN :
Book Description
Experiments on the Effects of Atmospheric Refraction and Airplane Accelerations on Sonic-boom Ground-pressure Patterns
Author : Domenic J. Maglieri
Publisher :
Page : 42 pages
File Size : 44,28 MB
Release : 1966
Category : Refraction
ISBN :
Book Description
A Summary of Results on Sonic-boom Pressure-signature Variations Associated with Atmospheric Conditions
Author : I. E. Garrick
Publisher :
Page : 27 pages
File Size : 23,48 MB
Release : 1968
Category :
ISBN :
Book Description
Subjective Response to Simulated Sonic Booms with Ground Reflections
Author : B. M. Sullivan
Publisher :
Page : 38 pages
File Size : 40,6 MB
Release : 1993
Category : Aerodynamic noise
ISBN :
Book Description
Sonic Boom Research
Author : A. R. Seebass
Publisher :
Page : 130 pages
File Size : 29,42 MB
Release : 1967
Category : Sonic boom
ISBN :
Book Description
Some Effects of Flight Path and Atmospheric Variations on the Boom Propagated from a Supersonic Aircraft
Author : Raymond L. Barger
Publisher :
Page : 36 pages
File Size : 47,46 MB
Release : 1964
Category : Aerodynamics
ISBN :
Book Description
Equations for the shock wave envelope and cusp line associated with the boom propagated from a supersonic aircraft are formulated in terms of the moving-trihedral coordinate system for flight in a uniform atmosphere and also in an atmosphere with a linear sound-speed gradient. Ray-tube theory is used to calculate the lateral distribution of boom intensity in an atmosphere with a linear sound-speed gradient and also to investigate the effect of a general wind and sound-speed gradient on the ground-track intensity. The relative effects of wind and temperature gradient are treated. The mechanism of focusing by winds and by ground structures are discussed qualitatively.
Some Nonasymptotic Effects on the Sonic Boom of Large Airplanes
Author : F. Edward McLean
Publisher :
Page : 28 pages
File Size : 47,34 MB
Release : 1965
Category : Meteorology in aeronautics
ISBN :
Book Description
Ground Measurements of Sonic-boom Pressures for the Altitude Range of 10,000 to 75,000 Feet
Author : Harvey H. Hubbard
Publisher :
Page : 56 pages
File Size : 19,50 MB
Release : 1964
Category : Sonic boom
ISBN :
Book Description
The U.S. Air Force, National Aeronautics and Space Administration, and Federal Aviation Agency have engaged in a joint research program for the purpose of measuring sonic-boom pressure signatures. These measurements are presented for several locations for flight tests of fighter and bomber airplanes in the altitude range from about 10,000 to 75,000 feet and at Mach numbers from 1.1 to 2.0. Data were obtained for a variety of atmospheric wind and temperature gradients and for various flight paths and acceleration rates.
Comparison of Measured and Calculated Sonic-boom Ground Patterns Due to Several Different Aircraft Maneuvers
Author : Donald L. Lansing
Publisher :
Page : 42 pages
File Size : 30,71 MB
Release : 1965
Category : Aeronautics in meteorology
ISBN :
