Electroforming Hardware for Aerospace Vehicles

2009 ◽  
pp. 124-124-16
Keyword(s):  
Aerospace Vehicles

A GENERALIZED LINEAR GUIDANCE LAW FOR AEROSPACE VEHICLES

1966 ◽  
Author(s):  
R. JOHNSON ◽  
C. LEONDES ◽  
J. PAYNE
Keyword(s):  
Aerospace Vehicles ◽  
Guidance Law

THE PROCESS OF NANOMODIFYING CAST ALUMINUM ALLOY INGOTS FOR COMPONENTS OF AEROSPACE VEHICLES

2019 ◽  
Vol 20 (2) ◽  
pp. 268-276
Author(s):  
G. G. Krushenko ◽  
◽  
V. P. Nazarov ◽  
S. N. Reshetnikova ◽  
G. V. Dvirnyi ◽  
...  
Keyword(s):  
Aluminum Alloy ◽  
Cast Aluminum Alloy ◽  
Cast Aluminum ◽  
Aerospace Vehicles

Dynamics of Aerospace Vehicles -- Nonlinear Flight Mechanics

2000 ◽  
Author(s):  
Jerry E. Jenkins ◽  
Gregory A. Addington ◽  
Phillip S. Beran ◽  
Deborah S. Grismer ◽  
Ernest S. Hanff
Keyword(s):  
Flight Mechanics ◽  
Aerospace Vehicles

MODERN MATERIALS IN THE CONSTRUCTION OF SENSORS FOR AEROSPACE VEHICLES

2020 ◽  
Author(s):  
A. P. Adamov ◽  
◽  
A. A. Adamova ◽  
S. G. Sementsov ◽  
◽  
...  
Keyword(s):  
Aerospace Vehicles

Control-oriented low-speed dynamic modeling and trade-off analysis of air-breathing aerospace vehicles

2019 ◽  
Vol 20 (12) ◽  
pp. 893-907
Author(s):  
Hai-dong Shen ◽  
Rui Cao ◽  
Yan-bin Liu ◽  
Fei-teng Jin ◽  
Yu-ping Lu
Keyword(s):  
Dynamic Modeling ◽  
Aerospace Vehicles ◽  
Trade Off ◽  
Air Breathing ◽  
Low Speed

Computational Fluid Dynamic Applications for Jet Propulsion System Integration

1991 ◽  
Vol 113 (1) ◽  
pp. 40-50 ◽  
Author(s):  
R. H. Tindell
Keyword(s):  
System Integration ◽  
Fluid Dynamic ◽  
Low Cost ◽  
Separated Flow ◽  
Propulsion System ◽  
Navier Stokes ◽  
Aerospace Vehicles ◽  
Design Engineers ◽  
Flow Phenomena ◽  
The Impact

The impact of computational fluid dynamics (CFD) methods on the development of advanced aerospace vehicles is growing stronger year by year. Design engineers are now becoming familiar with CFD tools and are developing productive methods and techniques for their applications. This paper presents and discusses applications of CFD methods used at Grumman to design and predict the performance of propulsion system elements such as inlets and nozzles. The paper demonstrates techniques for applying various CFD codes and shows several interesting and unique results. A novel application of a supersonic Euler analysis of an inlet approach flow field, to clarify a wind tunnel-to-flight data conflict, is presented. In another example, calculations and measurements of low-speed inlet performance at angle of attack are compared. This is highlighted by employing a simplistic and low-cost computational model. More complex inlet flow phenomena at high angles of attack, calculated using an approach that combines a panel method with a Navier-Stokes (N-S) code, is also reviewed. The inlet fluid mechanics picture is rounded out by describing an N-S calculation and a comparison with test data of an offset diffuser having massively separated flow on one wall. Finally, the propulsion integration picture is completed by a discussion of the results of nozzle-afterbody calculations, using both a complete aircraft simulation in a N-S code, and a more economical calculation using an equivalent body of revolution technique.

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