1967•Journal of AircraftRequires access
Limits on minimum speed V/STOL wind-tunnel tests.
William H. Rae
Open publisher page 21 citations
Abstract
body of revolution, far from the axis, Proc. Roy. Soc. (London) A201, 89-109 (March 1950). 8 Hubbard, H. H., Maglieri, D. J., Huckel, V., and Hilton, D. A. (with appendix by H. W. Carlson), Ground measurements of sonic-boom pressures for the altitude range of 10,000 to 75,000 feet, NASA TR R-198 (1964). (Supersedes NASA TM X-633.) 9 Walkden, F., The shock pattern of a wing-body combination, far from the flight path, Aeronaut. Quart. IX, Pt. 2, 164194 (May 1958). 10 Whitham, G. B.; The flow pattern of a supersonic projectile, Commun. Pure Appl. Math. V, 301-348 (August 1952). 11 Middle ton, W. D. and Carlson, H. W., A numerical method for calculating near-field sonic-boom pressure signatures, NASA TND-3082(1965). 12 Carlson, H. W., Mack, R, J., and Morris, O. A., Sonicboom pressure-field estimation techniques, J. Acoust. Soc. Am. (submitted for publication). 13 McLean, F. E. and Shrout, B. L., Design methods for minimization of sonic-boom pressure-field disturbances, J. Acoust. Soc. Am. (submitted for publication).