Add to ORKG"Calspan Report No. 6430-A-1.""Calspan Advanced Technology Center, Buffalo, New York.""Annual Report November 1, 1979 to November 1, 1980.""February 1981."Includes bibliographical references (page 36).Print reproduction.Air Force Contract No.Mode of access: Internet
"Final report: 15 March 1972 -- 15 May 1974.""June 1975."Includes bibliographical references (pages ...
Prepared at Langley Research Center."February 1966"--Cover.Includes bibliographical references (p. 2...
The flow-field structure in the vicinity and in the wake of an isolated 3D roughness element has bee...
"AGARDography 97, Part III.""Program Element 62405334, Project 8953, Task 895303.""May 1965."Include...
Measurements are given of the combined effects of two‐dimensional roughness and surface cooling on b...
Laminar turbulent transition is known for a long time as a critical phenomenon influencing the therm...
"This report is based on research sponsored by the U. S. Navy through the Office of Naval Research, ...
Prepared by Vought Aeronautics Company for Langley Research Center.N72-12225.Includes bibliographica...
"October 1964."Includes bibliograpical references (pages 86-91).Print reproduction.Air Force Contrac...
flw.This Final Report describes our research of hypersonic and supersonic boundary-layer In spite of...
"Final Technical Report from December 1, 1988 to March 1, 1990.""July 15, 1990."Includes bibliograph...
This project is based on Dr. Duan’s proposal, titled “Numerical Simulation of Freestream Acoustic Di...
This paper details the experimental study of roughness-induced boundary-layer transition in a hypers...
Condtions encountered in the high Mach number flow regime are show to profoundly affect the longitud...
This is a survey paper on the subject of hypersonic boundary-layer transition. Part 1 discusses boun...
"Final report: 15 March 1972 -- 15 May 1974.""June 1975."Includes bibliographical references (pages ...
Prepared at Langley Research Center."February 1966"--Cover.Includes bibliographical references (p. 2...
The flow-field structure in the vicinity and in the wake of an isolated 3D roughness element has bee...
"AGARDography 97, Part III.""Program Element 62405334, Project 8953, Task 895303.""May 1965."Include...
Measurements are given of the combined effects of two‐dimensional roughness and surface cooling on b...
Laminar turbulent transition is known for a long time as a critical phenomenon influencing the therm...
"This report is based on research sponsored by the U. S. Navy through the Office of Naval Research, ...
Prepared by Vought Aeronautics Company for Langley Research Center.N72-12225.Includes bibliographica...
"October 1964."Includes bibliograpical references (pages 86-91).Print reproduction.Air Force Contrac...
flw.This Final Report describes our research of hypersonic and supersonic boundary-layer In spite of...
"Final Technical Report from December 1, 1988 to March 1, 1990.""July 15, 1990."Includes bibliograph...
This project is based on Dr. Duan’s proposal, titled “Numerical Simulation of Freestream Acoustic Di...
This paper details the experimental study of roughness-induced boundary-layer transition in a hypers...
Condtions encountered in the high Mach number flow regime are show to profoundly affect the longitud...
This is a survey paper on the subject of hypersonic boundary-layer transition. Part 1 discusses boun...
"Final report: 15 March 1972 -- 15 May 1974.""June 1975."Includes bibliographical references (pages ...
Prepared at Langley Research Center."February 1966"--Cover.Includes bibliographical references (p. 2...
The flow-field structure in the vicinity and in the wake of an isolated 3D roughness element has bee...