ANOMALOUS HEAT TRANSFER AND PRESSURE DISTRIBUTIONS ON BLUNT BODIES AT HYPERSONIC SPEEDS IN THE PRESENCE OF AN IMPINGING SHOCK.

Technical Report · Mon Jan 01 00:00:00 EST 1968

DOI:https://doi.org/10.2172/4480948· OSTI ID:4480948

Edney, B.

• Research Organization: Flygtekniska Forsoksanstalten, Stockholm (Sweden)
• NSA Number: NSA-22-049015
• OSTI ID: 4480948
• Report Number(s): FFA-115
• Resource Relation: Other Information: UNCL. Orig. Receipt Date: 31-DEC-68
• Country of Publication: Country unknown/Code not available
• Language: English

Related Subjects

N24300* -Engineering-Heat Transfer & Fluid Flow
BODY
CONFIGURATION
DISTRIBUTION
HEAT TRANSFER
HYPERSONICS
MEASUREMENT
PRESSURE
SHOCK WAVES
SUPERSONICS
VELOCITY
PRESSURE/distribution on blunt bodies at hypersonic speeds
effects of impinging shock wave on
FLUID FLOW/heat transfer and pressure distribution on blunt bodies in hypersonic
effects of impinging shock wave on
SHOCK WAVES/effects of impinging
on heat transfer and pressure distribution on blunt bodies in hypersonic flow
HEAT TRANSFER/measurement of blunt body
in hypersonic flow
thin film gage for