Shock tunnel studies of high-enthalpy ionized airflows,

"AFOSR 3025."

Shock-bounded, self-similar flows with volumetric mass, momentum, and energy addition.

"DCAS-TDR-62-135. Report no. TDR-69 (2230-01)TR-2. Contract no. AF 04(695)-69."

An analysis of nonequilibrium inviscid flow,

"Air Force contract no. AF40(600)-928."

An experimental study of the effect of mass injection at the stagnation point of a blunt body,

"Army Ordnance contract no. DA-04-495-Ord-19."

Theoretical aerodynamics.

Mode of access: Internet.

Material presented at the NACA Conference on Supersonic Aerodynamics at Ames Aeronautical Laboratory on June 4, 1946, National Advisory Committee for Aeronautics.

Includes bibliography.

Supersonic aerodynamics and rocket propulsion,

Includes bibliographical references.

Investigation of ablation effects on hypersonic dynamic stability of a 10⁰ cone

Mode of access: Internet.

Comparison of turbulent wake characteristics with different eddy viscosity coefficients,

At head of title: Space Sciences Laboratory. Aerophysics Section.

A summary of similitude studies for high enthalpy hypersonic test facilities

Mode of access: Internet.

Investigation of test time at undertailored conditions in a shock tunnel.

Cover title.

Instrumentation studies for plasma jet and hypersonic wind tunnel,

"This research was supported by the McDonnell Aircraft Corporation under Contract no. 6140-20 P.O. 7S4899-R."

A variable atmosphere hypersonic wind tunnel for similitude studies

Mode of access: Internet.

Chord-wise air load distribution : War Dept., Army Air Forces : Navy Dept., Bureau of Aeronautics : Dept. of Commerce, Civil Aeronautics ... /

Tables.

Fluid dynamics and applications,

Reproduced from typewritten copy.