Studies of Airframe-propulsion-system Integration for Mach 6 Cruise Vehicles
Author:
Publisher:
Published: 1967
Total Pages: 26
ISBN-13:
DOWNLOAD EBOOKPosts
NASA Scientific and Technical Reports
Author: United States. National Aeronautics and Space Administration Scientific and Technical Information Division
Publisher:
Published: 1968
Total Pages: 428
ISBN-13:
DOWNLOAD EBOOKA Selected Listing of NASA Scientific and Technical Reports
Author: United States. National Aeronautics and Space Administration. Scientific and Technical Information Division
Publisher:
Published: 1968
Total Pages: 436
ISBN-13:
DOWNLOAD EBOOKScientific and Technical Aerospace Reports
Author:
Publisher:
Published: 1994
Total Pages: 1038
ISBN-13:
DOWNLOAD EBOOKGovernment-wide Index to Federal Research & Development Reports
Author:
Publisher:
Published: 1967-10
Total Pages: 1020
ISBN-13:
DOWNLOAD EBOOKConference on Hypersonic Aircraft Technology
Author:
Publisher:
Published: 1967
Total Pages: 590
ISBN-13:
DOWNLOAD EBOOKStudy of Hypersonic Propulsion/airframe Integration Technology
Author:
Publisher:
Published: 1978
Total Pages: 106
ISBN-13:
DOWNLOAD EBOOKInvestigation of Engine-exhaust-airframe Interference on a Cruise Vehicle at Mach 6
Author: James M. Cubbage
Publisher:
Published: 1971
Total Pages: 76
ISBN-13:
DOWNLOAD EBOOKResults from an investigation of the effects of underexpanded engine exhaust flow on the aerodynamic performance and stability of a cruise airplane at Mach 6 are presented. The influence of wing reflex angle and nozzle geometry on exhaust flow interference effects was investigated on a flat-plate model. The experiments were conducted at a free-stream Reynolds number of 17.05 X 10 (to the 6 power) based on the length of the airplane model over a model angle-of-attack range of 0(degrees) to 10(degrees) and at nozzle static-pressure ratios from 1 to approximately 4.
NASA Technical Memorandum
Author:
Publisher:
Published: 1992
Total Pages: 176
ISBN-13:
DOWNLOAD EBOOK