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."

Shock tunnel studies of high-enthalpy ionized airflows,

"AFOSR 3025."

Experimental studies of high temperature hypersonic diffusers.

"Project No. 1426. Task No. 142612."

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."

Tables of two-dimensional oscillating airfoil coefficients for rotary wings.

Mode of access: Internet.

Étude sur l'aviation,

Mode of access: Internet.

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

Loose-leaf.

Flight without formula : simple discussions on the mechanics of the aeroplane /

Mode of access: Internet.

Fluid-dynamic drag; practical information on aerodynamic drag and hydrodynamic resistance

Mode of access: Internet.

The resistance of the air and aviation experiments conducted at the Champ-de-Mars laboratory,

Mode of access: Internet.

NASA technical report.

Description based on: R-180; title from cover.

The slow motion of a permanently magnetized sphere in an electrically conducting medium,

"Research supported by the McDonnell Aircraft Corporation under Contract no. 6140-20 P.O. 7S4899-R and by the Purdue Research Foundation."

Airborne simulation for the SST.

Cover title.