The Aerothermodynamics of aircraft gas turbine engines /

Photocopy. [Springfield, Va. : National Technical Information Service, 1978]. -- 2 v.

Modulated entry /

"The technique of modulation, or variable coefficients, is discussed and the analytical formulation is reviewed. Representative numerical results of the use of modulation are shown for the lifting and nonlifting cases. These results include the effects of modulation on peak acceleration, entry corridor, and heat absorption. Results are given for entry at satellite speed and escape speed. The indications are that coefficient modulation on a vehicle with good lifting capability offers the possibility of sizable loading reductions or, alternatively, wider corridors; thus, steep entries become practical from the loading standpoint. The amount of steepness depends on the acceptable heating penalty. The price of sizable fractions of the possible gains does not appear to be excessive."

The carbon-carbon assessment program : appendix B, 50 MW ablation testing and results : [final report, May 73-March 74] /

Performing organization (under Contract or Grant no. F33615-71-C-1215): Aerotherm Division/Acurex Corporation.

Microstructural assessment of the series M 50MW ramp materials : final report for period April 1975 - June 1977 /

"AFML-TR-77-160."

Thermal buckling of solid wings.

"Contract no. Nonr 839 (18). Project No. NR 064-298."

Table and charts of equilibrium normal-shock and shock-tube properties for pure carbon dioxide with velocities from 1 to 16 km/sec /

Chiefly tables.

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."

Transport coefficients of air to 8000° K /

"29 September 1958."

Axisymmetric Hall-arc jet wind tunnel driver study

Mode of access: Internet.

Computer program for one-dimensional nonequilibrium reacting gas flow

Mode of access: Internet.

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

Mode of access: Internet.