Accession Number : AD0700863

Title :   SIMPLE FORMULAS FOR UNSTEADY PRESSURE ON SLENDER WEDGES AND CONES IN HYPERSONIC FLOW,

Corporate Author : NATIONAL AERONAUTICAL ESTABLISHMENT OTTAWA (ONTARIO)

Personal Author(s) : Orlik-Ruckemann,K. J.

Report Date : 22 JUL 1969

Pagination or Media Count : 5

Abstract : Simple formulas are presented with which the inviscid surface pressures at low frequencies can be rapidly calculated. It is also shown that for small amplitudes, the error introduced by omission of higher-order terms in frequency is generally less than 1% for reduced frequencies as high as 0.3. (Author)

Descriptors :   (*REENTRY VEHICLES, PRESSURE), HYPERSONIC CHARACTERISTICS, LOW FREQUENCY, SLENDER BODIES, WEDGES, CONICAL BODIES, OSCILLATION, CURVE FITTING, CANADA

Subject Categories : Aerodynamics
      Guided Missile Reentry Vehicles
      Fluid Mechanics

Distribution Statement : APPROVED FOR PUBLIC RELEASE