Proceedings of the SCAR Conference, held at Langley Research Center, Hampton, Virginia, November, 9-12, 1976. --

Includes bibliographical references.

La mécanique de l'aviation;

At head of title: R. Devillers ...

Hypersonic gas dynamic charts for equilibrium air /

Errata sheet inserted.

Aerothermodynamic consequences of nozzle nonequilibrium

"The research reported herein was...done by the Cornell Aeronautical Laboratory, Inc., for Arnold Engineering Development Center (AEDC) Air Force Systems Command (AFSC), under Program element 62405214, Project 6951, Task 695104."

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."

Stability of the boundary layer;

Reproduced from typewritten copy.

Vector polar method for shock interactions with area disturbances /

"AFOSR TN 59-701. Contract no. AF49(638)-166. I. E. R. project no. 96895."

Pressure gradient effects on supersonic boundary layer turbulence : final report /

"Carried out by the Fluid Mechanics Section of the Aeronutronic Division of the Ford Aerospace & Communications Corporation."

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."