A Survey of Unsteady Hypersonic Flow Problems

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Author(s)
Bisplinghoff, R. L.
Chawla, Jagannath P.
Morgan, Homer G.,
Runyan, Harry L.
and
Huckel, Vera
Runyan, Harry L.
and
Morgan, Homer G.
Hanson, Perry W.
Goete, Robert C.
Young, Lou S.
Bisplinghoff, R. L.
and
Ashley, Holt
Sewall, John L.,
Hess, Robert W.
and
Watkins, Charles E.
Morgan, Homer G.
Huckel, Vera
and
Runyan, Harry L.
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References (Appendix IV)
Title. etc.
Some structural and aeroelastic considerations of
high-speed flight.
19th Wright Brothers Lecture.
J.Ae.Sci. Vo1.23, No.4. April, 1956. pp.289-329.
Aeroelastio instability at high Maoh number.
J.Ae.Sci. Vo1.25, No.4. April, 1958. pp.246-258.
Theoretical considerations of flutter at high
Mach numbers.
J.Ae.Sci. Vo1.25, No.6. June, 1958. pp,371-331.
Flutter at very high speeds.
NASA TN D-942.
August, 1961.
Aerodynamio effects of sane configuration variables
on the aeroelastic characteristics of lifting
surfaces at Mach numbers from 0.7 to 6-86.
NASA TN D-984.
November, 1961.
Effects of leading-edge bluntness on flutter
characteristics of some square-planform doublewedge
airfoils at a Mach number of 15.4.
NASA TN D-1407.
October, 1962.
Effects of angle of attack and thickness ratio
on flutter of a rigid unswept diamond-airfoil
section dng at a Mach number of IO-O.
NASA TN D-1380.
August, 1962.
Principles of aercalasticity.
John Wiley & Sons Inc. 1962.
Analytical and experimental investigations of
flutter and divergence of spring mounted cone
configurations at supersonic speeds.
NASA TN D-1021.
April, 1962.
Procedure for calculating flutter athigh supersonic
speeds, including camber deflections, and
comparison with experimental results.
NACA TN 4335.
September, 1958.
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