Dynamic stability testing of aircraft—needs versus capabilities-Reference-Cited by-同舟云学术

Dynamic stability testing of aircraft—needs versus capabilities

Published:1975-01 Issue:4 Volume:16 Page:431-447
ISSN:0376-0421
Container-title:Progress in Aerospace Sciences
language:en
Short-container-title:Progress in Aerospace Sciences

Author:

Orlik-Rückemann K.J.

Publisher

Elsevier BV

Subject

Mechanical Engineering,Mechanics of Materials,Aerospace Engineering

Reference27 articles.

1. Effects of delta wing separation on shuttle dynamics;Reding;Journal of Spacecraft and Rockets,1973

2. Dynamic stability derivatives at angles of attack from −5° to 90° for a variable-sweep fighter configuration with twin vertical tails;Grafton;NASA TN D-6909,1972

3. Effects of a pointed nose on spin characteristics of a fighter airplane model including correlation with theoretical calculations;Chambers;NASA TN D-5921,1970

4. Dynamic stability derivatives of a twin-jet fighter model for angles of attack from −10° to 110°;Grafton;NASA TN D-6091,1971

5. Measurement of dynamic cross-derivatives due to pitching and yawing;Orlik-Rückemann;AIAA Paper 74–611,1974

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