Linearized theory of conical supersonic flow with application to triangular wings /

Loose-leaf.

Uniformly valid second-order solution for supersonic flow over cruciform surfaces,

"CM-1019."

Uniform second-order solution for supersonic flow over delta wing using reverse-flow integral method,

"CM-1034."

Reverse-flow integral methods for second-order supersonic flow theory,

"CM-1033."

The method of characteristics in compressible flow.

Reproduced from typewritten copy.

Investigation of the flow over simple bodies at Mach numbers of the order of 20 /

"It is shown that adequate means are available for calculating inviscid direct and induced pressures on simple axisymmetric bodies at zero angle of attack. The extent to which viscous effects can alter these predictions is indicated. It is also shown that inviscid induced pressures can significantly affect the stability of blunt, two-dimensional flat wings at low angles of attack. However, at high angles of attack, the inviscid induced pressure effects are negligible."

The blunt-body problem in hypersonic flow at low Reynolds number.

"Contract no. Nonr 2653(00)"

Low-flow and flow-duration data for Alabama streams.

Bibliography: p. 164.

Project bulletins nos. 1, 2, 3, and 4 : low-flow frequency analysis /

Mode of access: Internet.

Simulation of streamflow of Flambeau River at Park Falls, Wisconsin to define low-flow characteristics /

Prepared in cooperation with Wisconsin Department of Natural Resources.

Pilot study for storage requirements for low flow augmentation /

Mode of access: Internet.

Low-flow frequencies of Illinois streams,

Bibliography: p. 308.

The flow of a supersonic jet from a vessel with plane walls. Iztecheniye sverhzvookovoy strooi iz sosooda s ploskimi stenkami.

Translation of Istechenie sverkhzvukovoĭ strui iz sosuda s ploskimi stenkami (romanized form)

Low-flow transport models for conservative and sorbed solutes, Uvas Creek, near Morgan Hill, California /

Bibliography: p. 73-74.

Reverse flow and supersonic interference.

"AFOSR TN-58-625. ASTIA doc. no. AD 162 155."