Nonequilibrium scaling criterion for inviscid hypersonic airflows,

"Contract no. DA-30-069-ORD-3443. ARPA order no. 253-62."

A similitude for nonequilibrium phenomena in hypersonic flight,

"Part I of the present paper was supported by the Arnold Engineering Development Center under Contract no. AF-40-(601)-928. Part II is a part of project DEFENDER sponsored by the Advanced Research Projects Agency, Department of Defense, under Contract no. DA-30-069-ORD-3443."

Drag due to lift of a not-so-slender configuration; application of theory.

"Contract no. AF 33(616)-2933."

An investigation of laminar heat transfer to slender cones in the hypersonic shock tunnel

"Contract no. AF-33(616)-6025. Project no. 7064. Task no. 70169. Aeronautical Research Laboratory, Air Force Research Division, Air Research and Development Command, United States Air Force, Wright-Patterson Air Force Base."

A flight test comparison of take-off performance of two liaison type airplane configurations.

"Project no. 9-38-01-000 T 204, Contract no. DA 44-177- TC-462."

A correspondence between normal-shock and blunt-body flows,

"Contract no. DA-30-069-ORD-3443. ARPA order no. 253-62."

A theory of wing-propulsion combinations in slow flight.

"Project No. 9-38-01-00 Task 902. Contract No. DA 44177-TC-439. U. S. Army Transportation Research and Development Command, Transportation Corps, Fort Eustis, Virginia."

On the inviscid stability of the boundary layer on a flexible wall,

"This report is based on research sponsored by the U.S. Navy through the Office of Naval Research, Contract Nonr-2653(00)"

Vibration and dissociation coupling behind strong shock waves. Paper presented at the Symposium on Dynamics of Manned Lifting Planetary Entry,

Cover title.

Development of a method for predicting the performance and stresses of VTOL-type propellers.

"USAAVLABS technical report 66-26"

Shock tunnel studies of high-enthalpy ionized airflows,

"AFOSR 3025."

Comparison of aerodynamic stability derivatives obtained from analysis of F-100A dynamic lateral flight test data by two least squares methods.

Cover title.

The operations capacity of a runway used for landings and take-offs.

Cover title.

Mass flow measurement techniques for a flight enthalpy probe. Contract no. P.O.33-531174-G48.

Mode of access: Internet.

The upwash correction for an oscillating wing in a wind tunnel.

"Contract no. AF-33(038)-17848, study of dynamic stability model testing."