La mécanique de l'aviation;

At head of title: R. Devillers ...

Hypersonic gas dynamic charts for equilibrium air /

Errata sheet inserted.

Approximate solutions for nonequilibrium airflow in hypersonic nozzles,

Contract no. AF40(600)-804. AEDC TN-60-181. Arnold Engineering Development Center, Arnold Air Force Station, Tennessee. Air Research and Development Command, United States Air Force."

The aerodynamic appraisal of STOL/VTOL configurations,

"Project no. 9-38-01-000, Task 902; Contract no. DA 44-177-TC-439. U. S. Army transportation Research and Development Command, Transportation Corps, Fort Eustis, Virginia."

Skin friction, heat transfer, and pressure measurements on hypersonic inlet compression surfaces in the Mach number range 7.5 to 16.

Cornell Aeronautical Laboratory, Inc., Buffalo. Report no. AA-1948-Y-3

Experimental study of the effectiveness of cylindrical plume simulators for predicting jet-on boattail drag at Mach numberes up to 1.30 /

Prepared at Langley Research Center.

Investigation of helicopter rotor blade flutter and flapwise bending response in hovering

"Propulsion Laboratory, Contract no. AF33(616)-5210, Project no. 3137, Task no. 33113."

Theoretical analysis of the downstream influence of stagnation point mass transfer.

"Aeronautical Research Laboratory. Contract no. AF 33(616)-7064. Project no. 7064."

Bibliographical review of panel flutter and effects of aerodynamic noise

"Materials Laboratory, Contract no. AF 33(616)-5426, Project no. 7360."

Investigation of a method for the measurement of subsonic oscillatory aerodynamic influence coefficients,

"ASTIA document no. AD-142201."

Investigation of lateral stability at stall.

"Aeronautical Research Laboratory. Contract no. AF 33(038)-10480, RDO no. 472-106."

Stability of the boundary layer;

Reproduced from typewritten copy.

Boundary layer and wake modifications to compressor design systems : the effect of blade-to-blade flow variations on the mean flow field of a transonic rotor : final report, 01 September 1976-31 August 1978 /

"AFAPL-TR-79-2010."

The shock layer concept and three-dimensional hypersonic boundary layers.

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

Effects of ambient nonuniformities in flow over hypersonic test bodies.

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