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Force and pressure-distribution investigation to high angles of attack on all-movable triangular and rectangular wings in combination with a body at supersonic speedsForce and pressure distribution studies to high angles of attack on all-movable triangular and rectangular wings in combination with body at supersonic speeds
Document ID
19660024059
Acquisition Source
Legacy CDMS
Document Type
Other - NACA Research Memorandum
Authors
Hill, W. A., Jr. (NASA Ames Research Center Moffett Field, CA, United States)
Kaattari, G. E. (NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 2, 2013
Publication Date
July 10, 1956
Subject Category
Aerodynamics
Report/Patent Number
NACA-RM-A56C12
Report Number: NACA-RM-A56C12
Accession Number
66N33349
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
TRIANGULAR WING
RECTANGULAR WING
PRESSURE DISTRIBUTION
WING LOADING
ANGLE OF ATTACK
SUPERSONIC SPEED

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