A Survey of Unsteady Hypersonic Flow Problems

No
65
66
67
68
69
70
.
71
72
73
Author(s)
Dugundji, John,
and
Crisp, John 0. C.
Hanson, Perry W,
and
Doggett, Robert V.
Asher, Gifford W.
and
Watanabe, Roy K.
Van Dyke, Milton D.
Sylvester, Maurice A.
Hedgepeth, John Mb.
Shirk, Miohael H.
and
Olsen, James J.
Dixon, Sidney C.,
Griffith, George E.
ana
Bohon, Herman L.
Hess, Robert W.
and
Gibson, Frederick W.
74 Fag, Y. c.
- 76 -
Title, eto.
On the aeroelastic characteristics of low aspect
ratio wings with chordwise deformations.
Unpublished U.S. Report.
Aerodynamic damping of a 0.02 scale Saturn SA-1
Model vibrating in the first free-f?ee bending
mode.
NASA TN D-1956.
September, 1963.
Admittance techniques in high speed flutter model
testing. Part I.
WADD Tech. Report 61-31.
July, 1961.
A study of second order supersonic floiv theory.
NACA Report 1081. 1952.
Experimental studies of flutter of buckled
rectangular panels at Mach numbers from l-2 to
3.0 including effects of pressure differential
and of panel width length ratio.
NASA TN D-833.
May, 1961.
Flutter of rectangular simply supported panels
at high supersonic speeds.
J.Ae.Sci. Vo1.24, No.8. ~~-563573.
August, 1957.
.Reoent panel flutter research and application.
Paper presented at 17th Structures and Materials
Panel Meeting of AGARD.
A.R.C.26 337.
Experimental investigation at a Mach number of 3'0
of the effects of thermal stress and buckling
on the flutter of four-bay aluminium alloy panels
with length-width ratios of IO.
NASA TN D-921.
October, 1961.
Experimental investigation of the effeots of
compressive stress on the flutter of a curved
panel and a flat panel at supersonia Mach numbers.
NASA TN D-1306.
October, 1962.
Some recent oontributions to panel flutter research.
AIAA Journal, Vol.1, No.4.
April, 1963.
75./