Development of Atmospheric Gust Criteria for Supersonic Inlet Design
Title | Development of Atmospheric Gust Criteria for Supersonic Inlet Design PDF eBook |
Author | F. W. Barry |
Publisher | |
Pages | 212 |
Release | 1968 |
Genre | |
ISBN |
EFFECTS OF ATMOSPHERIC GUST CRITERIA ON SUPERSONIC INLET PERFORMANCE. 6TH CONFERENCE ON APPLIED METEOROLOGY. AMS/AIAA CONFERENCE ON AEROSPACE METEOROLOGY, LOS ANGELES/CALIF.1966
Title | EFFECTS OF ATMOSPHERIC GUST CRITERIA ON SUPERSONIC INLET PERFORMANCE. 6TH CONFERENCE ON APPLIED METEOROLOGY. AMS/AIAA CONFERENCE ON AEROSPACE METEOROLOGY, LOS ANGELES/CALIF.1966 PDF eBook |
Author | Frank W. Barry |
Publisher | |
Pages | 7 |
Release | 1966 |
Genre | |
ISBN |
Optimal Control of Supersonic Inlets to Minimize Unstarts
Title | Optimal Control of Supersonic Inlets to Minimize Unstarts PDF eBook |
Author | Bruce Lehtinen |
Publisher | |
Pages | 36 |
Release | 1971 |
Genre | Airplanes |
ISBN |
Design and characteristics of supersonic inlet controls for minimizing inlet unstarts.
NASA Technical Note
Title | NASA Technical Note PDF eBook |
Author | |
Publisher | |
Pages | 736 |
Release | 1973 |
Genre | Aeronautics |
ISBN |
NASA Conference Publication
Title | NASA Conference Publication PDF eBook |
Author | |
Publisher | |
Pages | 610 |
Release | 1978 |
Genre | Aeronautics |
ISBN |
Investigation of Fixed-geometry Supersonic Inlets with Bypass Ducts for Matching Turbojet-engine Air-flow Requirements Over a Range of Transonic and Supersonic Speeds
Title | Investigation of Fixed-geometry Supersonic Inlets with Bypass Ducts for Matching Turbojet-engine Air-flow Requirements Over a Range of Transonic and Supersonic Speeds PDF eBook |
Author | Abraham Leiss |
Publisher | |
Pages | 50 |
Release | 1958 |
Genre | Aerodynamics, Supersonic |
ISBN |
A method is presented to design a supersonic inlet that will match turbojet-engine air mass-flow requirements over a wide Mach number range. Two types of bypasses were investigated; one had a 360 degree annular cowling and the other had twin slotted ducts. Three models were flight tested. Two of the models, which had bypass ducts, were also ground tested. The bypass models had higher external drags. Both bypass models approximated a typical turbojet-engine air mass-flow requirement between Mach numbers 1.0 and 2.0. The flight tests covered a Reynolds number range from 200,000 to 800,000 and a Mach number range from 0.8 to 1.95.
Scientific and Technical Aerospace Reports
Title | Scientific and Technical Aerospace Reports PDF eBook |
Author | |
Publisher | |
Pages | 308 |
Release | 1991 |
Genre | Aeronautics |
ISBN |